Effect of a fuselage on delta wing vortex breakdown
Author:
Affiliation:
1. George Washington University, Hampton, Virginia 23681
2. Lockheed Engineering and Sciences Company, Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46600
Reference20 articles.
1. Fundamentals of Multivariate Analysis Part II. Inference About Two Treatments
2. Applying slender wing benefits to military aircraft
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2. Effect of Fuselage Cross Sections on Aerodynamic Characteristics of Reusable Launch Vehicles in Subsonic Flow;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2007
3. Wind-tunnel interference effects on a 70° delta wing;The Aeronautical Journal;2004-10
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