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Techniques for Tailoring Aircraft Stall and Post-Stall Behavior
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English
Abstract
This paper briefly reviews existing experimental and analytical techniques applied extensively to military configurations operating in stalled flight. As a consequence of these efforts, the fighter flight envelope has been expanded well beyond wing stall without encountering departures from controlled flight.
It is now also possible for engineering/mission trainer simulators to calculate all the motions an aircraft is capable of experiencing between -90° and +90° angle of attack. Exploiting these validated techniques relative to general aviation configurations could greatly influence Industry's future design and training efforts as well as FAA regulations and certification procedures.
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Authors
Citation
Bihrle, W., "Techniques for Tailoring Aircraft Stall and Post-Stall Behavior," SAE Technical Paper 931226, 1993, https://doi.org/10.4271/931226.Also In
References
- Bihrle William Jr. Bowman James S. Jr. Influence of Wing, Fuselage and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift Journal of Aircraft 18 11 November 1981
- Bihrle William Jr. Barnhart Billy Dickes Edward Influence of Forebody Geometry on Aerodynamic Characteristics and a Design Guide for Defining Departure/Spin Resistant Forebody Configurations WRDC TR 89-3079 September 1989
- Bihrle William Jr. Barnhart Billy Spin Prediction Techniques Journal of Aircraft 20 2 February 1983
- Bihrle William Jr. Prediction of High Alpha Flight Characteristics Utilizing Rotary Balance Data 13th Congress/AIAA Aircraft Systems and Technology Conference Proceedings August 1981
- Hultburg Randy S. Bowman James S. Jr. Martin Colin A. Measurements of Pressure on the Tail and Aft Fuselage of an Airplane Model during Rotary Motions at Spin Attitudes AIAA 88-4338-CP AIAA Atmospheric Flight Mechanics Conference August 15-17, 1988