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A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR … SHAMIYEH, ROTHFELD, HORNUNG 2 versatile activities to make the vision become reality. Among these activities, the design and devel-opment of a suitable aircraft is of central im- ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of MEASURES AND TEST TECHNIQUES FOR FUNGUS RESISTANCE TO Measures and Test Techniques for Fungus Resistance to Aircraft Materials and Equipment Table 2 Recommended coating Application object Ground Plating, coating and covering AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain CONCURRENT ENGINEERING DEVELOPMENT AND PRACTICES … 24TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES 1 Abstract Reduction of cycles (development time, series lead time) and costs along the aircraft lifecycle is a permanent priority. Concurrentengineering
PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), MINIMUM UNSTICK SPEED CALCULATION FOR HIGH-SPEED JET 24th INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES MINIMUM UNSTICK SPEED CALCULATION FOR HIGH-SPEED JET TRANSPORT AIRCRAFT R. Slingerland Faculty of CHALLENGES OF THE METALLIC FUSELAGE M. Pacchione, J. Telgkamp 4 skin of the upper fuselage in combination with bonded high strength 7349T7 / 7055T7 stringers. Furthermore,aluminum lithium
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR … SHAMIYEH, ROTHFELD, HORNUNG 2 versatile activities to make the vision become reality. Among these activities, the design and devel-opment of a suitable aircraft is of central im- ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of MEASURES AND TEST TECHNIQUES FOR FUNGUS RESISTANCE TO Measures and Test Techniques for Fungus Resistance to Aircraft Materials and Equipment Table 2 Recommended coating Application object Ground Plating, coating and covering AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain CONCURRENT ENGINEERING DEVELOPMENT AND PRACTICES … 24TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES 1 Abstract Reduction of cycles (development time, series lead time) and costs along the aircraft lifecycle is a permanent priority. Concurrentengineering
PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), MINIMUM UNSTICK SPEED CALCULATION FOR HIGH-SPEED JET 24th INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES MINIMUM UNSTICK SPEED CALCULATION FOR HIGH-SPEED JET TRANSPORT AIRCRAFT R. Slingerland Faculty of CHALLENGES OF THE METALLIC FUSELAGE M. Pacchione, J. Telgkamp 4 skin of the upper fuselage in combination with bonded high strength 7349T7 / 7055T7 stringers. Furthermore,aluminum lithium
ICAS - SECRETARIAT
The ICAS Secretariat is hosted by the German member society Deutsche Gesellschaft für Luft- und Raumfahrt. Axel Probst is the ICAS Executive Secretary. He is assisted by Bodo Heinrichs as ICAS Coordinator. c/o DGLR. Godesberger Allee 70. 53175 BONN, Germany. Phone: +49.228.3080519. Fax: +49.228.3080524. ICAS - PAPER LIBRARY Proceedings from congresses before 1998 were printed in thick bound paper volumes. These papers have been scanned and individual papers are available for download. The complete lists of content (as searchable pdf) from ICAS 1958 - ICAS 1996 can be downloaded via links below. We are working to make all papers available online. ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: MAL-PC40 Created Date: 11/30/2010 3:21:47 PM OUTLINE TECHNICAL PROGRAMME Aircraft Operation 1: 12:00 13:00: Lunch : 13:00 13:45: ICAS Casimiro Montenegro Filho Lecture for Innovation in Aeronautics - AGILE Project Consortium - Leitung: Michel Peters, ICAS EC Member, , NL 31TH ICAS CONGRESS 2018 ICAS 2018 - CD-ROM PROCEEDINGS INFORMATION FROM ICAS. ICAS 2018 Welcome About ICAS ICAS Member Societies and Associates ICAS Executive Committee, Programme Committee & ICAS 2018 Local Organizing Committee ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: kli Created Date: 10/20/2010 8:54:01 AM FLY-BY-WIRE AUGMENTED MANUAL CONTROL FLY-BY-WIRE AUGMENTED MANUAL CONTROL - BASIC DESIGN CONSIDERATIONS Dominik Niedermeier , Anthony A. Lambregts Deutsches Zentrum fürLuft-
REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENCE 3 REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENC E in several regions of influence, as sketched in Fig. 1. 2.1 Wing regions Wing regions, W-II and W-III are directly ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES ICAS - International Council of the Aeronautical Sciences THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC … 25TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC ACTUATORS, ACHIEVEMENTS AND LESSONS LEARNT Dominique van den Bossche Airbus Keywords: More Electric Aircraft, Flight Controls, Actuators, EHA Abstract For a long time the control surfaces of transport ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
ICAS - CALL FOR PAPERS/HANDLING The paperupload page for accepted papers for the 32nd ICAS congress in Shanghai can be found in your acceptance mail. Please visit this paper handling page for frequent updates concerning information about the upload/handling process of your abstract/paper. If you contact us via email always include your abstract/paper ID. A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR … SHAMIYEH, ROTHFELD, HORNUNG 2 versatile activities to make the vision become reality. Among these activities, the design and devel-opment of a suitable aircraft is of central im- ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the 2020 VISION: THE PROSPECTS FOR LARGE CIVIL AIRCRAFT ICAS 2000 CONGRESS 111.1 Abstract This paper will examine the prospects for propulsion systems for large civil transport aircraft over the next 2 decades, to the year AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain CONCURRENT ENGINEERING DEVELOPMENT AND PRACTICES … 24TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES 1 Abstract Reduction of cycles (development time, series lead time) and costs along the aircraft lifecycle is a permanent priority. Concurrentengineering
MEASURES AND TEST TECHNIQUES FOR FUNGUS RESISTANCE TO Measures and Test Techniques for Fungus Resistance to Aircraft Materials and Equipment Table 2 Recommended coating Application object Ground Plating, coating and covering ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
ICAS - CALL FOR PAPERS/HANDLING The paperupload page for accepted papers for the 32nd ICAS congress in Shanghai can be found in your acceptance mail. Please visit this paper handling page for frequent updates concerning information about the upload/handling process of your abstract/paper. If you contact us via email always include your abstract/paper ID. A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR … SHAMIYEH, ROTHFELD, HORNUNG 2 versatile activities to make the vision become reality. Among these activities, the design and devel-opment of a suitable aircraft is of central im- ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the 2020 VISION: THE PROSPECTS FOR LARGE CIVIL AIRCRAFT ICAS 2000 CONGRESS 111.1 Abstract This paper will examine the prospects for propulsion systems for large civil transport aircraft over the next 2 decades, to the year AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain CONCURRENT ENGINEERING DEVELOPMENT AND PRACTICES … 24TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES 1 Abstract Reduction of cycles (development time, series lead time) and costs along the aircraft lifecycle is a permanent priority. Concurrentengineering
MEASURES AND TEST TECHNIQUES FOR FUNGUS RESISTANCE TO Measures and Test Techniques for Fungus Resistance to Aircraft Materials and Equipment Table 2 Recommended coating Application object Ground Plating, coating and covering ICAS - PAPER LIBRARY Proceedings from congresses before 1998 were printed in thick bound paper volumes. These papers have been scanned and individual papers are available for download. The complete lists of content (as searchable pdf) from ICAS 1958 - ICAS 1996 can be downloaded via links below. We are working to make all papers available online. ICAS - CALL FOR PAPERS/HANDLING The paperupload page for accepted papers for the 32nd ICAS congress in Shanghai can be found in your acceptance mail. Please visit this paper handling page for frequent updates concerning information about the upload/handling process of your abstract/paper. If you contact us via email always include your abstract/paper ID. ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES ICAS - International Council of the Aeronautical Sciences REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENCE 3 REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENC E in several regions of influence, as sketched in Fig. 1. 2.1 Wing regions Wing regions, W-II and W-III are directly OUTLINE TECHNICAL PROGRAMME Aircraft Operation 1: 12:00 13:00: Lunch : 13:00 13:45: ICAS Casimiro Montenegro Filho Lecture for Innovation in Aeronautics - AGILE Project Consortium - Leitung: Michel Peters, ICAS EC Member, , NL ICAS 2008 OUTLINE PROGRAM ICAS 2008 OUTLINE PROGRAM ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES s f of Devices • res) that a interrax:e. Created Date. 8/7/201310:40:05 PM.
PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC … 25TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC ACTUATORS, ACHIEVEMENTS AND LESSONS LEARNT Dominique van den Bossche Airbus Keywords: More Electric Aircraft, Flight Controls, Actuators, EHA Abstract For a long time the control surfaces of transportICAS 2014 FINAL1
Title: Microsoft Word - ICAS 2014 Final1.doc Author: iberlow Created Date: 6/29/2014 15:58:2 ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
ICAS - CALL FOR PAPERS/HANDLING The paperupload page for accepted papers for the 32nd ICAS congress in Shanghai can be found in your acceptance mail. Please visit this paper handling page for frequent updates concerning information about the upload/handling process of your abstract/paper. If you contact us via email always include your abstract/paper ID. A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR … SHAMIYEH, ROTHFELD, HORNUNG 2 versatile activities to make the vision become reality. Among these activities, the design and devel-opment of a suitable aircraft is of central im- ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the 2020 VISION: THE PROSPECTS FOR LARGE CIVIL AIRCRAFT ICAS 2000 CONGRESS 111.1 Abstract This paper will examine the prospects for propulsion systems for large civil transport aircraft over the next 2 decades, to the year AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain CONCURRENT ENGINEERING DEVELOPMENT AND PRACTICES … 24TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES 1 Abstract Reduction of cycles (development time, series lead time) and costs along the aircraft lifecycle is a permanent priority. Concurrentengineering
MEASURES AND TEST TECHNIQUES FOR FUNGUS RESISTANCE TO Measures and Test Techniques for Fungus Resistance to Aircraft Materials and Equipment Table 2 Recommended coating Application object Ground Plating, coating and covering ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
ICAS - CALL FOR PAPERS/HANDLING The paperupload page for accepted papers for the 32nd ICAS congress in Shanghai can be found in your acceptance mail. Please visit this paper handling page for frequent updates concerning information about the upload/handling process of your abstract/paper. If you contact us via email always include your abstract/paper ID. A PERFORMANCE BENCHMARK OF RECENT PERSONAL AIR … SHAMIYEH, ROTHFELD, HORNUNG 2 versatile activities to make the vision become reality. Among these activities, the design and devel-opment of a suitable aircraft is of central im- ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the 2020 VISION: THE PROSPECTS FOR LARGE CIVIL AIRCRAFT ICAS 2000 CONGRESS 111.1 Abstract This paper will examine the prospects for propulsion systems for large civil transport aircraft over the next 2 decades, to the year AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain CONCURRENT ENGINEERING DEVELOPMENT AND PRACTICES … 24TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES 1 Abstract Reduction of cycles (development time, series lead time) and costs along the aircraft lifecycle is a permanent priority. Concurrentengineering
MEASURES AND TEST TECHNIQUES FOR FUNGUS RESISTANCE TO Measures and Test Techniques for Fungus Resistance to Aircraft Materials and Equipment Table 2 Recommended coating Application object Ground Plating, coating and covering ICAS - PAPER LIBRARY Proceedings from congresses before 1998 were printed in thick bound paper volumes. These papers have been scanned and individual papers are available for download. The complete lists of content (as searchable pdf) from ICAS 1958 - ICAS 1996 can be downloaded via links below. We are working to make all papers available online. ICAS - CALL FOR PAPERS/HANDLING The paperupload page for accepted papers for the 32nd ICAS congress in Shanghai can be found in your acceptance mail. Please visit this paper handling page for frequent updates concerning information about the upload/handling process of your abstract/paper. If you contact us via email always include your abstract/paper ID. ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES ICAS - International Council of the Aeronautical Sciences REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENCE 3 REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENC E in several regions of influence, as sketched in Fig. 1. 2.1 Wing regions Wing regions, W-II and W-III are directly OUTLINE TECHNICAL PROGRAMME Aircraft Operation 1: 12:00 13:00: Lunch : 13:00 13:45: ICAS Casimiro Montenegro Filho Lecture for Innovation in Aeronautics - AGILE Project Consortium - Leitung: Michel Peters, ICAS EC Member, , NL ICAS 2008 OUTLINE PROGRAM ICAS 2008 OUTLINE PROGRAM ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES s f of Devices • res) that a interrax:e. Created Date. 8/7/201310:40:05 PM.
PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC … 25TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES THE A380 FLIGHT CONTROL ELECTROHYDROSTATIC ACTUATORS, ACHIEVEMENTS AND LESSONS LEARNT Dominique van den Bossche Airbus Keywords: More Electric Aircraft, Flight Controls, Actuators, EHA Abstract For a long time the control surfaces of transportICAS 2014 FINAL1
Title: Microsoft Word - ICAS 2014 Final1.doc Author: iberlow Created Date: 6/29/2014 15:58:2 ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AGILE MANUFACTURING PROCESSES ICAS 2000 CONGRESS 591.1 AGILE MANUFACTURING PROCESSES Steve Timms, Tim Ogle, Mark Jackson, Chris Cooper BAE Systems Keywords: Agile, agility, lean, manufacturing, development, customer Abstract Agility is the next buzz-word for the aerospace PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON … IVO JEBACEK 2 1.1 Calibration of Strain Gauges Definition of a relation between forces (moments) effecting the wing and responses from strain gauges was needed for our purposes. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES ICAS 2000 CONGRESS 534.1 Industria de Turbo Propulsores, S.A. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES Daniel Ikaza Industria de Turbo Propulsores S.A. (ITP) PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), THE AERODYNAMIC DESI GN OF THE A350 XWB-900 HIGH LIFT … 1 . Abstract . The A350XWB -900 is the first member of the new family of Airbus long range high-lift aircraft. The development was launchedin 2006
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AGILE MANUFACTURING PROCESSES ICAS 2000 CONGRESS 591.1 AGILE MANUFACTURING PROCESSES Steve Timms, Tim Ogle, Mark Jackson, Chris Cooper BAE Systems Keywords: Agile, agility, lean, manufacturing, development, customer Abstract Agility is the next buzz-word for the aerospace PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON … IVO JEBACEK 2 1.1 Calibration of Strain Gauges Definition of a relation between forces (moments) effecting the wing and responses from strain gauges was needed for our purposes. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES ICAS 2000 CONGRESS 534.1 Industria de Turbo Propulsores, S.A. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES Daniel Ikaza Industria de Turbo Propulsores S.A. (ITP) PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), THE AERODYNAMIC DESI GN OF THE A350 XWB-900 HIGH LIFT … 1 . Abstract . The A350XWB -900 is the first member of the new family of Airbus long range high-lift aircraft. The development was launchedin 2006
ICAS - COUNCIL
C. Bil, Australia H. Deconinck, Belgium L. Santos de Brito Alvez, Brazil G. Languedoc,Canada J.C. Yao, China J. Juracka, Czech RepublicM. Kanerva, Finland
ICAS - PAPER LIBRARY Proceedings from congresses before 1998 were printed in thick bound paper volumes. These papers have been scanned and individual papers are available for download. The complete lists of content (as searchable pdf) from ICAS 1958 - ICAS 1996 can be downloaded via links below. We are working to make all papers available online. 2020 VISION: THE PROSPECTS FOR LARGE CIVIL AIRCRAFT ICAS 2000 CONGRESS 111.1 Abstract This paper will examine the prospects for propulsion systems for large civil transport aircraft over the next 2 decades, to the year ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: kli Created Date: 10/20/2010 9:05:56 AM FLY-BY-WIRE AUGMENTED MANUAL CONTROL FLY-BY-WIRE AUGMENTED MANUAL CONTROL - BASIC DESIGN CONSIDERATIONS Dominik Niedermeier , Anthony A. Lambregts Deutsches Zentrum fürLuft-
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: MAL-PC40 Created Date: 12/2/2010 3:33:56 PM ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: MAL-PC40 Created Date: 11/30/2010 3:21:47 PM CHALLENGES OF THE METALLIC FUSELAGE M. Pacchione, J. Telgkamp 4 skin of the upper fuselage in combination with bonded high strength 7349T7 / 7055T7 stringers. Furthermore,aluminum lithium
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL …TRANSLATE THISPAGE
ICAS - International Council of the Aeronautical Sciences REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENCE 3 REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENC E in several regions of influence, as sketched in Fig. 1. 2.1 Wing regions Wing regions, W-II and W-III are directly ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AGILE MANUFACTURING PROCESSES ICAS 2000 CONGRESS 591.1 AGILE MANUFACTURING PROCESSES Steve Timms, Tim Ogle, Mark Jackson, Chris Cooper BAE Systems Keywords: Agile, agility, lean, manufacturing, development, customer Abstract Agility is the next buzz-word for the aerospace PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON … IVO JEBACEK 2 1.1 Calibration of Strain Gauges Definition of a relation between forces (moments) effecting the wing and responses from strain gauges was needed for our purposes. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES ICAS 2000 CONGRESS 534.1 Industria de Turbo Propulsores, S.A. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES Daniel Ikaza Industria de Turbo Propulsores S.A. (ITP) PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), THE AERODYNAMIC DESI GN OF THE A350 XWB-900 HIGH LIFT … 1 . Abstract . The A350XWB -900 is the first member of the new family of Airbus long range high-lift aircraft. The development was launchedin 2006
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCESMEMBERSNEXT EVENTSICAS ORGHISTORYCOOPERATIONSARCHIVE The ICAS organisation consists of two corporate bodies, the Council (being the assembly of Member Societies), having all authority other than the authority given to others according to the law or these Statutes and the Executive Committee, responsible for the management of ICAS. The Council appoints the Executive Committee for a two yearperiod.
AIR INTAKES : ROLE, CONSTRAINTS AND DESIGN AIR INTAKES: ROLE, CONSTRAINTS AND DESIGN 643.3 FIGURE 2 3.5 Design With all of the constraints, which are generally aerodynamic, air intakes can be designed which will of ELECTROMECHANICAL ACTUATOR ( EMA ) ADVANCED TECHNOLOGIES 3 Electromechanical actuator (EMA) advanced technologies for flight controls At the moment, a large part of potential solutions under development is concentrated on AGILE MANUFACTURING PROCESSES ICAS 2000 CONGRESS 591.1 AGILE MANUFACTURING PROCESSES Steve Timms, Tim Ogle, Mark Jackson, Chris Cooper BAE Systems Keywords: Agile, agility, lean, manufacturing, development, customer Abstract Agility is the next buzz-word for the aerospace PREDICTIVE & DETECTIVE MAINTENANCE R. B. PARRA, J. C. de ALMEIDA Jr 2 ideas about the concepts of aeronautical maintenance, from the first fruits of preventive maintenance, that served as a basis for the AN OVERVIEW OF THE DE-ICING AND ANTI-ICING TECHNOLOGIES 3 AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES WITH PROSPECTS FOR THE FUTURE 28 29 3 2 2 14 3 3 5 2 4 3 1 3 3 7 Loss of control in flight CFIT* *CFIT = Controlled Flight Into Terrain MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON … IVO JEBACEK 2 1.1 Calibration of Strain Gauges Definition of a relation between forces (moments) effecting the wing and responses from strain gauges was needed for our purposes. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES ICAS 2000 CONGRESS 534.1 Industria de Turbo Propulsores, S.A. THRUST VECTORING NOZZLE FOR MILITARY AIRCRAFT ENGINES Daniel Ikaza Industria de Turbo Propulsores S.A. (ITP) PROPELLER BLADE ELEMENT MOMENTUM THEORY WITH … PROPELLER BLADE ELEM 3 ENT MOMENTUM THEORY WITH VORTEX WAKE DELFECTION An axial induction factor, a, is customarily defined as, V=V ∞ (1+a) (1.6) and from Equation (1.5), THE AERODYNAMIC DESI GN OF THE A350 XWB-900 HIGH LIFT … 1 . Abstract . The A350XWB -900 is the first member of the new family of Airbus long range high-lift aircraft. The development was launchedin 2006
ICAS - COUNCIL
C. Bil, Australia H. Deconinck, Belgium L. Santos de Brito Alvez, Brazil G. Languedoc,Canada J.C. Yao, China J. Juracka, Czech RepublicM. Kanerva, Finland
ICAS - PAPER LIBRARY Proceedings from congresses before 1998 were printed in thick bound paper volumes. These papers have been scanned and individual papers are available for download. The complete lists of content (as searchable pdf) from ICAS 1958 - ICAS 1996 can be downloaded via links below. We are working to make all papers available online. 2020 VISION: THE PROSPECTS FOR LARGE CIVIL AIRCRAFT ICAS 2000 CONGRESS 111.1 Abstract This paper will examine the prospects for propulsion systems for large civil transport aircraft over the next 2 decades, to the year ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: kli Created Date: 10/20/2010 9:05:56 AM FLY-BY-WIRE AUGMENTED MANUAL CONTROL FLY-BY-WIRE AUGMENTED MANUAL CONTROL - BASIC DESIGN CONSIDERATIONS Dominik Niedermeier , Anthony A. Lambregts Deutsches Zentrum fürLuft-
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: MAL-PC40 Created Date: 12/2/2010 3:33:56 PM ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES Author: MAL-PC40 Created Date: 11/30/2010 3:21:47 PM CHALLENGES OF THE METALLIC FUSELAGE M. Pacchione, J. Telgkamp 4 skin of the upper fuselage in combination with bonded high strength 7349T7 / 7055T7 stringers. Furthermore,aluminum lithium
ICAS - INTERNATIONAL COUNCIL OF THE AERONAUTICAL …TRANSLATE THISPAGE
ICAS - International Council of the Aeronautical Sciences REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENCE 3 REVIEW OF PROPELLER-WING AERODYNAMIC INTERFERENC E in several regions of influence, as sketched in Fig. 1. 2.1 Wing regions Wing regions, W-II and W-III are directlyContact:
ICAS(at)ICAS.org
WELCOME TO ICAS
"COVERING THE WORLD OF AERONAUTICS" ICAS is an international, non-government, non-profit scientific organization with the mission to advance knowledge and facilitate collaboration in aeronautics. ICAS is the only international support organization to representative aeronautical engineering professional societies and their members in 30 countries. ICAS organizes every two years an International Congress covering all aspects of aeronautical science and technology and their application to both military and civil aviation. An official presentation about ICAS can be downloaded(here) .
-------------------------Note on Covid19:
The International Council of the Aeronautical Sciences is highly aware of the Covid19 situation, but as of now, there is no plan to cancel or postpone the ICAS 2020 Congress in Shanghai. We strongly hope that the situation will be solved long before September. However we are staying vigilant and provide frequent updates. Everyone’s safety is our primary concern. Please check our website regularly: www.icas2020.com The preliminary programme isonline
A more detailed part of the technical programme can be found here.
------------------------- The paper templates (Word and LaTex) for the 2020 ICAS congress in Shanghai is now available. Please visit our Paper Handling page for moreinformation.
------------------------- The winners of the prestigious ICAS awards for 2020 have beenannounced.
Media release download ------------------------- The acceptance/rejection mails have been sent out 8th November 2019. If you haven't received them (2 mails) please check your SPAM folder. In case you still haven't received anything, especially if you submitted with an email adress of Northwestern Polytechnical University where we encountered problems sending the mails, please contact the Secretariat. If your abstract was selected as a reserve paper please refrain from sending emails about becoming an active oral presentation. If and when that would happen we obviously cannot tell but you'll get the information as soon as your paper moves up to an activepresentation.
------------------------- The ICAS Emerging Technology Forum 2019 (9th-10th September in Melbourne, Australia) was open for the public. Please see the website for updated information and programme information.
Also see the report on our webpage . ------------------------- THE CALL FOR PAPERS FOR THE 2020 ICAS CONGRESS IN SHANGHAI, CHINA ISCLOSED.
IF YOU ABSTRACT WAS ACCEPTED PLEASE VISIT OUR CALL FOR PAPERS PAGE FOR MORE INFORMATION ABOUT UPLOADING AND HANDLING OF YOUR PAPER. ------------------------- The official ICAS YouTube channelhas been
launched, there you'll find some information about ICAS and ourcongresses.
------------------------- The very successful congress was held in Belo Horizonte from 9th to 14th September 2018. We would like to thank all authors/presenters, session chairs, and supporting people who made this congress such a success. Please see the short videoabout
the event.
We hope to see you again in Shanghai, China in 2020 ------------------------- ICAS 2018 FINAL PROGRAMME/PROCEEDINGS The final programme/Proceedings are available in our congress library.
The ISBN number after publishing in the national library is978-3-932182-88-4 .
All the general and award lectures can be found on our congress reportpage .
------------------------- The ICAS 2020 Congress will be held in Shanghai, China. General information is available at:www.icas2020.com
------------------------- FOR FURTHER INFORMATION PLEASE CONTACTIN COOPERATION WITH
ICAS Secretariat
c/o DGLR
Godesberger Allee 70 53175 BONN, Germany Phone: +49.228.3080519 Fax: +49.228.3080524 E-mail: icas(at)icas.orgMember societies
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