Design requirements for the NASA Langley supersonic low-disturbance wind tunnel-Reference-Cited by-同舟云学术

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Design requirements for the NASA Langley supersonic low-disturbance wind tunnel

Published:1986-03-05 Issue: Volume: Page:
ISSN:
Container-title:14th Aerodynamic Testing Conference
language:
Short-container-title:

Author:

BECKWITH I.¹,CHEN F.-J.¹,CREEL, JR. T.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-763

Reference22 articles.

1. H a r v e y , W. D.; S t a i n b a c k , P. C.: A n d e r s , J . B.: and C a r y , A. M.: N o z z l e W a l l B o u n d a r y - L a y e r T r a n s i t i o n a n d F r e e s t r e a m D i s t u r b a n c e s a t Mach 5. AIAA J o u r n a l . V o l . 13, No. 3, M a r c h 1 9 7 5 , pp. 307-314.

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3. Numerical investigation of the application of porous material in tandem nozzle supersonic wind tunnels;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

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