Blockage Corrections for Blunt-Based Bodies of Revolution-Reference-Cited by-同舟云学术

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Blockage Corrections for Blunt-Based Bodies of Revolution

Published:1966-04 Issue:664 Volume:70 Page:532-533
ISSN:0368-3931
Container-title:The Journal of the Royal Aeronautical Society
language:en
Short-container-title:J. R. Aeronaut. Soc.

Author:

Calvert J. R.

Abstract

Maskell has developed a theory for the blockage effects of bluff bodies in a closed wind tunnel and has shown that it gives good results for flat plates normal to a stream. For streamline bodies there are well established methods of calculating the corrections, but for long bodies with blunt bases it is not obvious what method should be used.

Publisher

Cambridge University Press (CUP)

Reference3 articles.

1. Maskell E. C. A theory of the blockage effects on bluff bodies and stalled wings in a closed wind tunnel. ARC R & M 3400, 1965.

2. Evans J. Y. G. Corrections to velocity for wall constraint in any 10 x 7 rectangular subsonic wind tunnel. ARC R. & M 2662, 1953.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Subsonic axisymmetric base flow experiments with base modifications;Journal of Spacecraft and Rockets;1980-01

2. Reduction of Base Drag by Boat-Tailed Afterbodies in Low-Speed Flow;Aeronautical Quarterly;1969-11

3. Blockage Corrections for Blunt-Based Bodies of Revolution;The Aeronautical Journal;1968-12

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