Comment on 'Effect of fuselage on delta wing vortex breakdown'
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46601
Reference8 articles.
1. Effect of a fuselage on delta wing vortex breakdown
2. Equivalent angle-of-attack method for estimating nonlinear aerodynamics of missile fins
3. Unique high-alpha roll dynamics of a sharp-edged 65 deg delta wing
4. Further analysis of high-rate rolling experiments of a 65 deg delta wing
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1. Further analysis of self-induced roll oscillations of a non-slender delta wing;The Aeronautical Journal;2006-11
2. Analysis of Self-Induced Roll Oscillations of a 45-Degree Delta Wing;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
3. Multifaceted Influence of Fuselage Geometry on Delta-Wing Aerodynamics;Journal of Aircraft;2003-01
4. From Water Tunnel to Poststall Flight Simulation: The F/A-18 Investigation;Journal of Aircraft;2002-11
5. Multifaceted influence of fuselage geometry on delta wing aerodynamics;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14
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