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The requirements for a new full scale subsonic wind tunnelJustification and requirements are presented for a large subsonic wind tunnel capable of testing full scale aircraft, rotor systems, and advanced V/STOL propulsion systems. The design considerations and constraints for such a facility are reviewed, and the trades between facility test capability and costs are discussed.
Document ID
19720011641
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kelly, M. W. (NASA Ames Research Center Moffett Field, CA, United States)
Mckinney, M. O. (NASA Ames Research Center Moffett Field, CA, United States)
Luidens, R. W. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1972
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-62106
Report Number: NASA-TM-X-62106
Accession Number
72N19291
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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