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X-29A for NTF wind-tunnel/flight correlationsConsiderations and recommendations for correlation are given. Basic tunnel calibration prior to research and development tests is suggested. Areas of concentration include: wing cruise drag and drag rise, wing separation and stall, afterbody and base drag, propulsion effects, vortex flows, cavity flows, and excrescences.
Document ID
19820017334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Daforno, G. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Publication Information
Publication: NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981
Subject Category
Aerodynamics
Accession Number
82N25210
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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