Reynolds number effects on a supersonic transport at transonic conditions-Reference-Cited by-同舟云学术

Reynolds number effects on a supersonic transport at transonic conditions

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Wahls R.¹,Owens L.¹,Rivers S.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-912

Reference54 articles.

1. AIAA-2001-0912

2. 23 967. 20.03 120.6 oa 20.03 994. 20.61 -97.21

3. 83 1003. 20.78 -184.0

4. 00 1755. 36.30 -52.07 1.1 79.61 1797. 37.29 -249.4

5. .0 80.00!\C.0 120.78 963. 19.98 120.2 995. 20.63 -97.26 1005. 20.82 -184.2 1755. 36.32 -52.16 1802. 37.32 -249.1 2677. 55.50 -185.2 2704. 56.11 -250.5 b) Transonic cruise configurationwith nacelles.

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