Calibration of the Langley 8-Foot High Temperature Tunnel for hypersonic airbreathing propulsion testing-Reference-Cited by-同舟云学术

Calibration of the Langley 8-Foot High Temperature Tunnel for hypersonic airbreathing propulsion testing

Published:1996-06-17 Issue: Volume: Page:
ISSN:
Container-title:Advanced Measurement and Ground Testing Conference
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Author:

Huebner Lawrence¹,Rock Kenneth¹,Voland Randall¹,Wieting Allan¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2197

Reference27 articles.

1. Methane-Air Combustion Gases as an Aerodynamic Test Medium

2. Reubush, D. E.; Puster, R. L.; and Kelly, H.N. "Modification to the Langley 8-Foot High Temperature Tunnel for Hypersonic Propulsion Testing,"AIAAPaper 87-1887,June 1987.

3. Perrell, E. R.: Computation of Combustion Heated Hypersonic Wind Tunnel Flows in Phase Nonequilibrium, Ph.D. Thesis,North Carolina StateUniversity, 1994.

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