Contour Design Techniques for Super/Hypersonic Wind Tunnel Nozzles-Reference-Cited by-同舟云学术

Contour Design Techniques for Super/Hypersonic Wind Tunnel Nozzles

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Shope Frederick¹

Affiliation:

1. Aerospace Testing Alliance

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3665

Reference17 articles.

1. A History of Aerodynamics

2. 3Sivells, J. C. "A Computer Program for the Aerodynamic Design of Axisymmetric and Planar NozzlesforSupersonicandHypersonicWind Tunnels,"AEDC-TR-78-63,Dec.1978.

3. 5Johnson, C. B., and Boney, L. R. "A Method for Calculating a Real-Gas Two-Dimensional Nozzle ContourIncluding the EffectsofGamma," NASA TMX-3243, Sep.1975.

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