Open AccessCALCULATION OF STEADY PLANE AND AXISYMMETRIC SUPERSONIC GAS FLOWS CONTAINING AN ARBITRARILY LARGE NUMBER OF SHOCKS.
Author(s) -
David B. Taylor
Publication year - 1968
Publication title -
osti oai (u.s. department of energy office of scientific and technical information)
Language(s) - English
Resource type - Reports
DOI - 10.2172/4798090
Subject(s) - supersonic speed , rotational symmetry , mechanics , plane (geometry) , physics , classical mechanics , mathematics , geometry
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