Inviscid design of hypersonic wind tunnel nozzles for a real gas-Reference-Cited by-同舟云学术

Inviscid design of hypersonic wind tunnel nozzles for a real gas

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Korte J.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-677

Reference7 articles.

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2. 21 0 10 1 41 49 61 32 0 -1 -1 10 0 -21 13 Case 1: Real gas design, downstream section-supersonic. R-Gas-l 0

3. 400 1716.563 1.000 .896 0.2273-07 .ooo .ooo 1000.000 12.000 3.000 .OOO 1x.200 14.000 -48.91131 -1.000 10.000 41 21 0 10 -1 41 49 61 32 0 -1 -1 10 0 -21 13 Case 2: Ideal gas design, supersonic contour. I-Gas-2 0

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