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Interaction Effects Produced by Jet Exhausting Laterally Near Base of Ogive-Cylinder Model in Supersonic Main StreamThe experimentally determined interaction effects of a side jet exhausting near the base of an ogive-cylinder model are presented and discussed. The interaction force appears to be independent of main-stream Mach number, boundary-layer condition (laminar or turbulent), angle of attack, and forebody length. The ratio of interaction force to jet force is found to be inversely proportional to the square root of the product of jet stagnation-to-free-stream pressure ratio and jet-to-body diameter ratio.
Document ID
19980232077
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Vinson, P. W. (Michigan Univ. Ann Arbor, MI United States)
Amick, J. L. (Michigan Univ. Ann Arbor, MI United States)
Liepman, H. P. (Michigan Univ. Ann Arbor, MI United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1959
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-MEMO-12-5-58W
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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