An Engineering Inviscid-Reacting Boundary Layer Method for Calculation of Hypersonic Aerodynamic Heating
43rd:; meeting.; MEETING AND EXHIBIT, Aerospace sciences ; 2005 ; Reno, NV
2005-01-01
AIAA 2005-510
2005-0019 - 2005-1421 with gaps
Conference paper
English
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Engineering Interactive Inviscid Boundary-Layer Method for Hypersonic Flow
Online Contents | 1995
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