Vortex-wake characteristics of a supersonic transport wing planform at Mach 2.5
Author:
Affiliation:
1. Polytechnic University, Brooklyn, New York 11201
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13303
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1. Features and problems of experimental study of supersonic vortex flows;HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2019): Proceedings of the XXVI Conference on High-Energy Processes in Condensed Matter, dedicated to the 150th anniversary of the birth of S.A. Chaplygin;2019
2. The synthesis of polyolefin graft copolymers by reactive extrusion;Progress in Polymer Science;1999-04
3. Interaction of Wing Vortices and Plumes in Supersonic Flight;IUTAM Symposium on Dynamics of Slender Vortices;1998
4. Broadband Vibration Damping Using Highly Distributed Tuned Mass Absorbers;AIAA Journal;1997-04
5. Near-Field Experiments on Tip Vortices at Mach 3.1;AIAA Journal;1997-04
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