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Investigation of the Flow Through a Single-stage Two-dimensional Nozzle in the Langley 11-inch Hypersonic Tunnel
Document ID
19930082869
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mclellan, Charles H
Williams, Thomas W
Beckwith, Ivan E
Date Acquired
August 16, 2013
Publication Date
December 1, 1950
Report/Patent Number
NACA-TN-2223
Report Number: NACA-TN-2223
Accession Number
93R12159
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - HYPERSONIC (11")
NOZZLES, HIGH-PRESSURE
FLOW - NOZZLES
WIND TUNNELS - AIR FLOW
WIND TUNNEL APPARATUS - NACA - HYPERSONIC (11")
WIND TUNNELS - PRESSURE
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