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Comments on V/STOL wind tunnel data at low forward speeds.V/STOL wind tunnel data at low forward speeds, discussing test limit dependence on model size, downwash angle and tunnel geometry
Document ID
19690057240
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rae, W. H., Jr.
Shindo, S.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Publication Information
Publisher: CORNELL AERONAUTICAL LAB., INC.,
Subject Category
Facilities, Research, And Support
Meeting Information
Meeting: AERODYNAMICS OF ROTARY WING AND V/STOL AIRCRAFT, SYMPOSIUM
Location: BUFFALO, NY
Start Date: June 18, 1969
End Date: June 20, 1969
Sponsors: CORNELL AERONAUTICAL LAB. AND U.S. ARMY AVIATION MATERIEL LABS.
Accession Number
69A35229
Funding Number(s)
CONTRACT_GRANT: DA-ARO/D/-31-124-G934
CONTRACT_GRANT: NGR-48-002-035
CONTRACT_GRANT: DA-ARO/D/-31-124-G809
CONTRACT_GRANT: DA-ARO/D/-31-124-G481
Distribution Limits
Public
Copyright
Other

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