Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing-Reference-Cited by-同舟云学术

Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing

Published:2001-04 Issue:11 Volume:79 Page:1077-1088
ISSN:0045-7949
Container-title:Computers & Structures
language:en
Short-container-title:Computers & Structures

Author:

Smith A.L.,Mee D.J.,Daniel W.J.T.,Shimoda T.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,General Materials Science,Modelling and Simulation,Civil and Structural Engineering

Reference10 articles.

1. Rae WH, Pope A. Low-speed wind tunnel testing. New York: Wiley; 1984

2. Drag balance for hypervelocity impulse facilities;Sanderson;AIAA J,1991

3. Finite element modelling of a three-component force balance for hypersonic flows;Daniel;Comput Struct,1995

4. Three-component force balance for flows of millisecond duration;Mee;AIAA J,1996

5. Shirouzu M, Wantanabe S, Suzuki H, Yamamoto M, Morito T. A quick report of the hypersonic flight experiment, HYFLEX. 20th International Symposium on Space Technology and Science, Gifu, Japan, 19–25 May, 1996

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