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An experimental investigation of delta wing vortex flow with and without external jet blowingA visual and quantitative study of the vortex flow field over a 70-deg delta wing with an external jet blowing parallel to and at the leading edge was conducted. In the experiment, the vortex core was visually marked with TiCl4, and LDA was used to measure the velocity parallel and normal to the wing surface. It is found that jet blowing moved vortex breakdown farther downstream from its natural position and influenced the breakdown characteristics.
Document ID
19890037703
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Iwanski, Kenneth P.
(U.S. Navy, Naval Coastal Systems Center Panama City, FL, United States)
Ng, T. Terry
(Eidetics International, Inc. Torrance, CA, United States)
Nelson, Robert C.
(Notre Dame, University IN, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-0084
Accession Number
89A25074
Funding Number(s)
CONTRACT_GRANT: NCA2-162
Distribution Limits
Public
Copyright
Other

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