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A Study of Second-Order Supersonic Flow TheorySecond-order solutions of supersonic-flow problems are sought by iteration, using the linearized solution as the first step. For plane and axially symmetric flows, particular solutions of the iteration equation are discovered which reduce the second-order problem to an equivalent linearized problem. Comparison of second-order solutions with exact and numerical results shows great improvement over linearized theory. For full three-dimensional flow, only a partial particular solution is found. The inclined cone is solved, and the possibility of treating more general problems is considered.
Document ID
19930090965
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Van Dyke, Milton D
Date Acquired
September 6, 2013
Publication Date
January 1, 1952
Report/Patent Number
NACA-TR-1081
Accession Number
93R20255
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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