NASA NTRS · 19730016558
Computer programs for predicting supersonic and hypersonic interference flow fields and heating
Abstract
This report describes computer codes which calculate two-dimensional shock interference patterns. These codes compute the six types of interference flows as defined by Edney (Aeronaut. Res. Inst. of Sweden FAA Rep. 115). Results include properties of the inviscid flow field and the inviscid-viscous interaction at the surface along with peak pressure and peak heating at the impingement point.
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Morris, D. J., Keyes, J. W.. 1973-05-01. Computer programs for predicting supersonic and hypersonic interference flow fields and heating. https://ntrs.nasa.gov/citations/19730016558
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