Numerical Study of Energy Deposition Requirements for Aerodynamic Control of Hypersonic Vehicles-Reference-Cited by-同舟云学术

Numerical Study of Energy Deposition Requirements for Aerodynamic Control of Hypersonic Vehicles

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bisek Nicholas¹,Boyd Iain¹,Poggie Jonathan²

Affiliation:

1. University of Michigan

2. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1109

Reference30 articles.

1. Laminar-Turbulent Transition in a Mach 8 Elliptic Cone Flow

2. 2Nowlan, D., Burke, A., and Bird, K. “Pressure and Heat Transfer Distribution on ASD Elliptic Cone (W3) and ASD Sortie (W4) in the CAL 48-Inch Hypersonic Shock Tunnel,” CAL Report AM-1800-Y-2, December 1963. ASC94 2649

3. Flow control using various plasma and aerodynamic approaches (Short review)

4. Mechanisms of plasma actuators for hypersonic flow control

5. Aerodynamically blunt and sharp bodies

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