Transonic wind-tunnel flows about a fully configured model of aircraft-Reference-Cited by-同舟云学术

Transonic wind-tunnel flows about a fully configured model of aircraft

Published:1995-03 Issue:3 Volume:33 Page:557-559
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Takakura Yoko¹,Ogawa Satoru²,Wada Yasuhiro²

Affiliation:

1. Tokyo Noko University, Tokyo 184, Japan

2. National Aerospace Laboratory, Tokyo 182, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.12497

Reference10 articles.

1. ^non. "Experimental Data Base for Computer Program Assessment, Report of the Fluid Dynamics Panel Working Group 04," AGARD Rept. AR-138,1979.

2. A 3-D chimera grid embedding technique

3. 4Takakura, Y., and Ogawa, S. "Computations of Transonic Flows about a Fully Configured Model of Aircraft Using a Multi-Domain Technique," Computers and Fluids (to be published).

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