Use of an expansion tube to examine scramjet combustion at hypersonic velocities-Reference-Cited by-同舟云学术

Use of an expansion tube to examine scramjet combustion at hypersonic velocities

Published:1989-07-12 Issue: Volume: Page:
ISSN:
Container-title:25th Joint Propulsion Conference
language:
Short-container-title:

Author:

RIZKALLA O.¹,BAKOS R.¹,PULSONETTI M.¹,CHINITZ WALLACE¹,ERDOS JOHN¹

Affiliation:

1. General Applied Science Laboratories, Inc., Ronkonkoma, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-2536

Reference16 articles.

1. Hypervelocity Aerodynamics with Chemical Nonequilibrium

2. Supersonic hydrogen combustion with a short thrust nozzle

3. (c) Stalker. R.J.'Developmentof a Hypervelocity Wind Tunnel." Aeronautical J., Vol.76, pp.374-384,June 1972. 3. Anderson,G.Y. "An Outlook onHypersonic

4. Flight,''AIAA Preprint No. 87-2074,June 1987. 4.Trimpi. R.L."A Preliminary Theoretical

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