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The numerical calculation of inviscid plume flow fieldsA numerical method is presented for the computation of inviscid, axisymmetric, underexpanded plumes. The numerical techniques developed by Moretti (1969, 1971, 1972) are used in conjunction with Abbett's (1970) theory for locating the Mach disk. Abbett's theory and three other prediction methods are compared to experimental results. Results are presented for jets exhausting into static ambients and supersonic free stream. Detailed results from a flow field with multiple Mach disks are also presented. Finally, some problems associated with the computation of very small Mach disks are discussed.
Document ID
19740050370
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salas, M. D.
(Grumman Aerospace Corp., Bethpage, N.Y.; NASA, Langley Research Center Configurations and Performance Section, Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
June 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 74-523
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Palo Alto, CA
Start Date: June 17, 1974
End Date: June 19, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A33120
Distribution Limits
Public
Copyright
Other

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