Nonequilibrium Effects on Prediction of Aerothermodynamic Loading for a Double Cone-Reference-Cited by-同舟云学术

Nonequilibrium Effects on Prediction of Aerothermodynamic Loading for a Double Cone

Published:2019-07 Issue:7 Volume:57 Page:2946-2963
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Kianvashrad Nadia¹,Knight Doyle D.¹

Affiliation:

1. Rutgers University, New Brunswick, New Jersey 08901

Funder

Emil Buehler Foundation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057883

Reference49 articles.

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2. SippelM.SchwanekampT.TrivailoO.LentschA. “Progress of SpaceLiner Rocket-Powered High-Speed Concept,” DLR, German Aerospace Center TR IAC-13-D2.4.05, Sept. 2013, http://elib.dlr.de/87329/ [retrieved 2019].

3. Simulation of Hypersonic Shock Wave Laminar Boundary Layer Interaction on Hollow Cylinder Flare, Part II

4. Hypersonic Mach number and real gas effects on Space Shuttle Orbiteraerodynamics

5. “STS-1 Anomaly Report,” NASA Tech. Rept. SSVEO IFA List Feb. 2003, OV-103, Columbia, 2003.

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