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Dynamic Pressure Equations Used at the 14- by 22-Foot Subsonic TunnelThis document provides a description of equations used to calculate test section dynamic pressure in the 14- by 22-Foot Subsonic Tunnel. The equation used to calculate dynamic pressure is dependent on the test section configuration.
Document ID
20190018049
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Quinto, P. Frank (NASA Langley Research Center Hampton, VA, United States)
Boney, Andy D. (Jacobs Technology, Inc. Hampton, VA, United States)
Date Acquired
May 10, 2019
Publication Date
May 6, 2019
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NF1676L-32662
Report Number: NF1676L-32662
Funding Number(s)
WBS: 478076.07.05
Distribution Limits
Public
Copyright
Public Use Permitted.

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