A combustion driven shock tunnel to complement the free piston shocktunnel T5 at GALCIT-Reference-Cited by-同舟云学术

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A combustion driven shock tunnel to complement the free piston shocktunnel T5 at GALCIT

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

BELANGER JACQUES¹,HORNUNG HANS¹

Affiliation:

1. California, Institute of Technology, Pasadena

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3968

Reference4 articles.

1. STANJAN Chemical Equilibrium Solver, (c) StanfordUniversity,V3.89VAX.1987.

2. Hypersonic Shock Tunnel

3. (3)Bklanger,J."DescriptionandUseofaComputer Program for Unsteady One-Dimensional Calculations of Shock Tunnel Processes". GALCITReportFM-90-3,October 1990.

4. Lordi J.A., Mates R.E. and Moselle J.R. "ComputerProgram for the Numerical Solution of Nonequilibrium Expansions of Reacting Gas Mixtures". NASA Contractor report CR-472, May 1966.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis of factors determining numerical solution in the calculation of flow with combustion using the ONERA experimental model;Thermophysics and Aeromechanics;2023-10-23

2. A New Combustion-Driver 1.1 m Diameter Hypersonic Shock Tunnel to Simulate Mach 10 Flight Conditions;25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2023-05-27

3. Performance data of the new free-piston shock tunnel at GALCIT;28th Joint Propulsion Conference and Exhibit;1992-07-06

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