NASA NTRS · 19780019140
Computer programs for calculating two-dimensional potential flow in and about propulsion system inlets
Abstract
Incompressible potential flow calculations are presented that were corrected for compressibility in two-dimensional inlets at arbitrary operating conditions. Included are a statement of the problem to be solved, a description of each of the computer programs, and sufficient documentation, including a test case, to enable a user to run the program.
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Hawk, J. D., Stockman, N. O., Farrell, C. A., Jr.. 1978-06-01. Computer programs for calculating two-dimensional potential flow in and about propulsion system inlets. https://ntrs.nasa.gov/citations/19780019140
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