Static And Rotational Aerodynamic Data From O To 90 Angle Of Attack For A Series Of Basic And Altered Forebody Shapes

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Static And Rotational Aerodynamic Data From O To 90 Angle Of Attack For A Series Of Basic And Altered Forebody Shapes

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Author : William Bihrle (Jr)
language : en
Publisher:
Release Date : 1989

Static And Rotational Aerodynamic Data From O To 90 Angle Of Attack For A Series Of Basic And Altered Forebody Shapes written by William Bihrle (Jr) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Airplanes categories.

The loss of airplanes and occupants attributable to departures from controlled flight and ensuing spins has been a problem since the earliest days of aviation. These losses have plagued both the military and general aviation communities. The phenomena responsible for such losses take on added significance because, in the past ten years, high angle-of-attack capability in the post-stall region has been shown to significantly enhance the air combat maneuvering effectiveness of fighter airplanes and, therefore, this is not a region to be avoided, but rather exploited, if possible. Fortunately, the aerodynamic characteristics that produce departures and spins have been identified within the past few years through rotary balance tests, which identify an airplane's aerodynamic characteristics in a steady rotational flow environment. It was demonstrated in the Phase I that the high angle-of-attack aerodynamic characteristics are very configuration dependent and that forebody geometry can have a significant influence on these characteristics. In the extreme case, an aircraft's undesirable aerodynamics can be completely attributable to the forebody. In this instance, autorotative yawing and rolling moments, as well as increasing nose-up pitching moments with increasing rotation rate, are realized.

Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1990

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aeronautics categories.

Influence Of Forebody Geometry On Aerodynamic Characteristics And A Design Guide For Defining Departure Spin Resistant Forebody Configurations

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Author : William Bihrle (Jr)
language : en
Publisher:
Release Date : 1989

Influence Of Forebody Geometry On Aerodynamic Characteristics And A Design Guide For Defining Departure Spin Resistant Forebody Configurations written by William Bihrle (Jr) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Airplanes categories.

The loss of airplanes and occupants attributable to departures from controlled flight and ensuing spins has been a problem since the earliest days of aviation. These losses have plagued both the military and general aviation communities. The phenomena responsible for such losses take on added significance because, in the past ten years, high angle-of-attack capability in the post-stall region has been shown to significantly enhance the air combat maneuvering effectiveness of fighter airplanes and, therefore, this is not a region to be avoided, but rather exploited, if possible. Fortunately, the aerodynamic characteristics that produce departures and spins have been identified within the past few years through rotary balance tests, which identify an airplane's aerodynamic characteristics in a steady rotational flow environment. It was demonstrated in the Phase I that the high angle-of-attack aerodynamic characteristics are very configuration dependent and that forebody geometry can have a significant influence on these characteristics. In the extreme case, an aircraft's undesirable aerodynamics can be completely attributable to the forebody. In this instance, autorotative yawing and rolling moments, as well as increasing nose-up pitching moments with increasing rotation rate, are realized.

Proceedings Of The Non Linear Aero Prediction Requirements Workshop

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Author : Michael J. Logan
language : en
Publisher:
Release Date : 1994

Proceedings Of The Non Linear Aero Prediction Requirements Workshop written by Michael J. Logan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Airplanes categories.

Aiaa 28th Aerospace Sciences Meeting

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Author :
language : en
Publisher:
Release Date : 1990

Aiaa 28th Aerospace Sciences Meeting written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aeronautics categories.

Government Reports Annual Index

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Author :
language : en
Publisher:
Release Date : 199?

Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 199? with categories.

Nasa Conference Publication

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Author :
language : en
Publisher:
Release Date : 1994

Nasa Conference Publication written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.

Government Reports Announcements Index

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Author :
language : en
Publisher:
Release Date : 1990

Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Science categories.

Static And Rotational Aerodynamic Data From O Deg To 90 Deg Angle Of Attack For A Series Of Basic And Altered Forebody Shapes

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Author :
language : en
Publisher:
Release Date : 1989

Static And Rotational Aerodynamic Data From O Deg To 90 Deg Angle Of Attack For A Series Of Basic And Altered Forebody Shapes written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with categories.

This report contains static and rotational aerodynamic data from 0 to 90 degrees angle of attack for a series of basic and altered forebody shapes. (jhd).

92 4338 To 92 4494

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Author :
language : en
Publisher:
Release Date : 1992

92 4338 To 92 4494 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Aerodynamics categories.