1. Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
2. 2New World Vistas: Air and Space Powerfor the 21stCentury, Aircraft and Propulsion Vol., AirForce Scientific AdvisoryBoard,Washington,DC,Dec.1995,pp.66-67.
3. 4VanDyke,M.,AnAlbumof Fluid Motion, ParabolicPress, Stanford, CA, 1982.
4. 5Berry,S.A.,Horvath,T.J.,Kowalkowski,M.K.,andLiechty,D.S."X-33(Rev-F)Aeroheating Results of Test 6770in NASA Langley 20-inch Mach 6 AirTunnel,"NASA/TM1999-209122,March 1999.