Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic A Nasa

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Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic And Transonic Speeds

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Author : John E. Lamar
language : en
Publisher:
Release Date : 2001

Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic And Transonic Speeds written by John E. Lamar and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with Airplanes categories.

Geometrical, flight, computational fluid dynamics (CFD), and wind-tunnel studies for the F-16XL-1 airplane are summarized over a wide range of test conditions. Details are as follows: (1) For geometry, the upper surface of the airplane and the numerical surface description compare reasonably well. (2) For flight, CFD, and wind-tunnel surface pressures, the comparisons are generally good at low angles of attack at both subsonic and transonic speeds; however, local differences are present. In addition, the shock location at transonic speeds from wind-tunnel presure contours is near the aileron hinge line and generally is in correlative agreement with flight results.

Nasa Technical Paper

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Author :
language : en
Publisher:
Release Date :

Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.

Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic A Nasa

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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 2003*

Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic A Nasa written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003* with categories.

Innovation In Flight

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Author : Joseph R. Chambers
language : en
Publisher:
Release Date : 2005

Innovation In Flight written by Joseph R. Chambers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2005 with Aeronautics categories.

Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic And Transonic Speeds

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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-06-15

Flight Wind Tunnel And Computational Fluid Dynamics Comparison For Cranked Arrow Wing F 16xl 1 At Subsonic And Transonic Speeds written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-06-15 with categories.

Geometrical, flight, computational fluid dynamics (CFD), and wind-tunnel studies for the F-16XL-1 airplane are summarized over a wide range of test conditions. Details are as follows: (1) For geometry, the upper surface of the airplane and the numerical surface description compare reasonably well. (2) For flight, CFD, and wind-tunnel surface pressures, the comparisons are generally good at low angles of attack at both subsonic and transonic speeds, however, local differences are present. In addition, the shock location at transonic speeds from wind-tunnel pressure contours is near the aileron hinge line and generally is in correlative agreement with flight results. (3) For boundary layers, flight profiles were predicted reasonably well for attached flow and underneath the primary vortex but not for the secondary vortex. Flight data indicate the presence of an interaction of the secondary vortex system and the boundary layer and the boundary-layer measurements show the secondary vortex located more outboard than predicted. (4) Predicted and measured skin friction distributions showed qualitative agreement for a two vortex system. (5) Web-based data-extraction and computational-graphical tools have proven useful in expediting the preceding comparisons. (6) Data fusion has produced insightful results for a variety of visualization-based data sets. Lamar, John E. and Obara, Clifford J. and Fisher, Bruce D. and Fisher, David F. Armstrong Flight Research Center; Langley Research Center RTOP 522-31-31-03

Monthly Catalog Of United States Government Publications

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Author :
language : en
Publisher:
Release Date : 2003

Monthly Catalog Of United States Government Publications written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003 with Government publications categories.

Nasa Langley Scientific And Technical Information Output 2001

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Author :
language : en
Publisher:
Release Date : 2002

Nasa Langley Scientific And Technical Information Output 2001 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with categories.

40th Aiaa Aerospace Sciences Meeting Exhibit

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Author :
language : en
Publisher:
Release Date : 2002

40th Aiaa Aerospace Sciences Meeting Exhibit written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Aeronautics categories.

Airplane Aerodynamics And Performance

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Author : Jan Roskam
language : en
Publisher: DARcorporation
Release Date : 1997

Airplane Aerodynamics And Performance written by Jan Roskam and has been published by DARcorporation this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Science categories.

Flying Beyond The Stall

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Author : Douglas A. Joyce
language : en
Publisher:
Release Date : 2014

Flying Beyond The Stall written by Douglas A. Joyce and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014 with Research aircraft categories.

The X-31 Enhanced Fighter Maneuverability Demonstrator was unique among experimental aircraft. A joint effort of the United States and Germany, the X-31 was the only X-plane to be designed, manufactured, and flight tested as an international collaboration. It was also the only X-plane to support two separate test programs conducted years apart, one administered largely by NASA and the other by the U.S. Navy, as well as the first X-plane ever to perform at the Paris Air Show. Flying Beyond the Stall begins by describing the government agencies and private-sector industries involved in the X-31 program, the genesis of the supermaneuverability concept and its initial design breakthroughs, design and fabrication of two test airframes, preparation for the X-31's first flight, and the first flights of Ship #1 and Ship #2. Subsequent chapters discuss envelope expansion, handling qualities (especially at high angles of attack), and flight with vectored thrust. The book then turns to the program's move to NASA's Dryden Flight Research Center and actual flight test data. Additional tasking, such as helmet-mounted display evaluations, handling quality studies, aerodynamic parameter estimation, and a "tailless" study are also discussed.The book describes how, in the aftermath of a disastrous accident with Ship #1 in 1995, Ship #2 was prepared for its outstanding participation in the Paris Air Show. The aircraft was then shipped back to Edwards AFB and put into storage until the late 1990s, when it was refurbished for participation in the U. S. Navy's VECTOR program. The book ends with a comprehensive discussion of lessons learned and includes an Appendix containing detailed information.