Similarity for high-angle-of-attack subsonic/transonic slender-body aerodynamics
Author:
Affiliation:
1. PRC Aerospace Technologies Division, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45723
Reference15 articles.
1. Engineering analysis of slender-body aerodynamics using Sychev similarity parameters
2. Three-dimensional hypersonic gas flow past slender bodies at high angles of attack
3. Extension of hypersonic, high-incidence, slender-body similarity
4. Lifting-Line Theory of Oblique Wings in Transonic Flows
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2. Surface pressure model for simple delta wings at high angles of attack;Sadhana;2001-12
3. Symmetry breaking in vortical flows over cones - Theory and numerical experiments;AIAA Journal;1994-05
4. Symmetry breaking in vortical flows over cones - Theory and numerical experiments;11th Applied Aerodynamics Conference;1993-08-09
5. Hypersonic Slender Body Theory for All Angles of Attack;Astrodynamics Conference;1992-08-10
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