This paper has established the models calculating aero-optic effect of the hypersonic flying vehicle, and using a new turbulence hypothesis model, which is on base of Johnson- King & k-(epsilon) equation. Then the calculating program was designed. In the last part, the calculating result was discussed.
Calculating aero-optic effect of turbulent flow on the hypersonic flying vehicle
Propagation and Imaging through the Atmosphere IV ; 2000 ; San Diego,CA,United States
Proc. SPIE ; 4125
17.11.2000
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Calculating aero-optic effect of turbulent flow on the hypersonic flying vehicle [4125-11]
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