Some compressibility effects on the lee side flow structures of cruciform wing–body configurations with very low aspect ratio wings
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference36 articles.
1. A multi-vortex method for axisymmetric bodies at angle of attack;Angelucci;J. Aircr.,1971
2. Symmetric vortex separation on circular cylinders and cones;Bryson;Appl. Mech.,1959
3. Stability of symmetric vortices in two dimensions and over three-dimensional slender conical bodies;Cai;J. Fluid Mech.,2003
4. Stability of vortex pairs over slender conical bodies: Analysis and numerical computation;Cai;AIAA J.,2003
5. A physical mechanism for vortex merging;Cerretelli;J. Fluid Mech.,2003
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1. Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack;Fluid Dynamics;2020-09
2. On the supersonic flow over an axisymmetric step at an angle of attack;AIP Conference Proceedings;2018
3. Two-Dimensional Potential Method Simulations of a Body–Strake Configuration;Journal of Spacecraft and Rockets;2014-03
4. An Engineering Method for Very Low Aspect Ratio Cruciform Wing-Body Configurations;31st AIAA Applied Aerodynamics Conference;2013-06-22
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