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A critical examination of expansion tunnel performanceAn experimental study of the performance of the expansion tunnel for various test gases and range of quiescent acceleration section and nozzle pressure, nozzle geometric area ratio, and nozzle axial station has been performed. Flow diagnostics used to examine expansion tunnel flow characteristics were time histories and profiles of pitot pressure and axial component of flow velocity. The purpose of this study was to determine experimentally what limitations might restrict predicted operational flexibility and the advantages and disadvantages of this mode of operation as compared to the expansion tube. Results are presented which demonstrate the expansion tunnel offers several advantages over the expansion tube, but the severity of the disadvantages of the tunnel makes the expansion tube mode of operation the more desirable for performing hypersonic-hypervelocity aerothermodynamic studies of proposed entry configurations.
Document ID
19780048420
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Miller, C. G.
(NASA Langley Research Center Space Systems Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 78-768
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: San Diego, CA
Start Date: April 19, 1978
End Date: April 21, 1978
Accession Number
78A32329
Distribution Limits
Public
Copyright
Other

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