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Investigation of a Two-step Nozzle in the Langley 11-inch Hypersonic Tunnel
Document ID
19930082782
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mclellan, Charles Herbert
Williams, Thomas W
Bertram, Mitchel H
Date Acquired
August 16, 2013
Publication Date
September 1, 1950
Report/Patent Number
NACA-TN-2171
Accession Number
93R12072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIR FLOW - NOZZLES
WIND TUNNELS - AIR FLOW
PHOTOGRAPHY - AIR FLOW - NOZZLES
WIND TUNNELS - NACA - HYPERSONIC (11 INCHES)
WIND TUNNEL TESTS - NACA - HYPERSONIC (11 INCHES)
BOUNDARY LAYER - NOZZLES
WIND TUNNELS, HYPERSONIC
NOZZLES, HIGH-PRESSURE
SCHLIEREN METHOD
WIND TUNNELS - PRESSURE

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