High-alpha aerodynamics of a slender tailless aircraft
Author:
Affiliation:
1. Inst. for Aerospace Research, Ottawa, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-94
Reference12 articles.
1. ^ddington, G. A. and Myatt, J. HL, 'Control-Surface Deflection Effects on Aerodynamic Response Nonlinearities,"AIAAPaper 2000-4107,Aug.2000.
2. 3Beyers, M. E. andEricsson, L. E. ''Rotary Aerodynamics of a Slender Tailless Aircraft Configuration," to be published.
3. 4Hanff, E. S. and Jenkins, S. B. "Large Amplitude High Rate Roll Experiments on a DeltaWing andDouble-Delta Wing,"AIAA Paper 90-0224,Jan. 1990.
4. Effect of Fuselage Geometry on Delta-Wing Vortex Breakdown
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