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Flow-field in a vortex with breakdown above sharp edged delta wingsThe behavior of vortex-flow, accompanied with breakdown, formed above sharp-edged delta wings, was studied experimentally as well as theoretically. Emphasis is placed particularly on the criterion for the breakdown at sufficiently large Reynolds numbers
Document ID
19790003846
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hayashi, Y. (NASA Headquarters Washington, DC United States)
Nakaya, T. (NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-75339
NAL-TR-423
Report Number: NASA-TM-75339
Report Number: NAL-TR-423
Accession Number
79N12017
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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