1. Numerical prediction of the reflection plate boundary layer effects on half plane model in wind tunnel
2. Kumar, S. "CFD Study of Sting Effect - Stage 1," Technical Report in IAR, Sep. 1999. 3. 1. Su and J.T. Conway, "Numerical Analysis of the Aerodynamics of the Aurora Aircraft by an Inviscid/Viscous Interaction Method," 22ndInternational Congress of Aeronautical Sciences, Aug. 2000, Harrogate, UK. 4. http://flash.icemcfd.comlindex.htrnl 5. NPARC User's Guide- NASA LeRClAEDC Alliance, Version 3.0, Sep. 1996. Washington. 6. Cooper, G. K. and Sirbaugh, 1. R. "ParcCode: Theory and Usage," AEDC-TR-89-15,Sverdrup Technolgy Inc.
3. Figure 3. PressureCoefficient Differences Between TwoConfigurations, M.=0.564, a=O.O
4. Figure 5(t) 1.9 -1.2
5. 8-0.2