Control of High-Angle-of-Attack Reentry Flow with Plasma Actuators-Reference-Cited by-同舟云学术

Control of High-Angle-of-Attack Reentry Flow with Plasma Actuators

Published:2013-03 Issue:2 Volume:50 Page:337-346
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Atkinson Michael¹,Poggie Jonathan¹,Camberos José¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32360

Reference50 articles.

1. Re-Entry Aerodynamics

2. High Angle-of-Attack Aerodynamics

3. Hypersonic viscous flows over sphere-cones at high angles of attack

4. StetsonK. “Experimental Results of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack at M∞=14.2,” Aerospace Research Lab. TR-71-0127, Aug. 1971.

5. NowlanD. “Pressure and Heat Transfer Distribution on ASD Elliptic Cone (W3) and ASD Sortie (W4) in the CAL 48-Inch Hypersonic Shock Tunnel,” Cornell Aeronautical Lab Rept. TR-AM-1800-Y-2, 1964.

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