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The rationale and design features for the 40 by 80/80 by 120 foot wind tunnelA substantial increase in the test capability of full scale wind tunnels is considered. In order to determine the most cost effective means for providing this desired increase in test capability, a series of design studies were conducted of various new facilities as well as of major modifications to the existing 40- by 80-foot wind tunnel. The most effective trade between test capability and facility cost was provided by repowering the existing 40 by 80 foot wind tunnel to increase the maximum speed from 200 knots to 300 knots and by the addition of a new 80- by 120-foot test section having a 110 knot maximum speed. The design of the facility is described with special emphasis on the unique features, such as the drive system which absorbs nearly four times the power without an increase in noise, and the large flow diversion devices required to interface the two test sections to a single drive.
Document ID
19760018135
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mort, K. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Kelly, M. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Hickey, D. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: AGARD Wind Tunnel Design and Testing Tech.
Subject Category
Research And Support Facilities (Air)
Accession Number
76N25223
Distribution Limits
Public
Copyright
Other
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