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A perforated-wall nozzle for variable Mach number testing.Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests
Document ID
19680058556
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hendershot, K. C.
Martin, J. F.
Sheeran, W. J.
Date Acquired
August 4, 2013
Publication Date
September 1, 1968
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 68-238
Report Number: AIAA PAPER 68-238
Meeting Information
Meeting: FLIGHT TEST, SIMULATION AND SUPPORT CONFERENCE
Location: LOS ANGELES, CA
Start Date: March 25, 1968
End Date: March 27, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A39528
Funding Number(s)
CONTRACT_GRANT: NAS8-20027
Distribution Limits
Public
Copyright
Other

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