NASA NTRS · 19770026220
Improved computer programs for calculating potential flow in propulsion system inlets
Abstract
Computer programs to calculate the incompressible potential flow corrected for compressibility in axisymmetric inlets at arbitrary operating conditions are presented. Included are a statement of the problem to be solved, a description of each of the programs and sufficient documentation, including a test case, to enable a user to run the programs.
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Stockman, N. O., Farrell, C. A., Jr.. 1977-07-01. Improved computer programs for calculating potential flow in propulsion system inlets. https://ntrs.nasa.gov/citations/19770026220
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