Research is being conducted on the numerical simulation of transonic flow around a low noise short takeoff and landing (STOL) experimental aircraft, Asuka. The purposes of this research are to evaluate the high speed aerodynamic characteristics of the Asuka, to evaluate the aerodynamic interference between the elements and airframe according to the parametric study, and to construct a numeric data base.
Numerical Simulation of Transonic Flow Around Asuka
1987
2 pages
Report
No indication
English
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