<--- Back to Details
| First Page | Document Content | |
|---|---|---|
 Date: 2007-09-17 12:10:26Dynamics Scramjet Combustor Shock wave Ramjet Mach number Pressure measurement Rayleigh flow Unstart Jet engines Aerospace engineering Fluid dynamics |
Add to Reading List |
Microsoft Word - VSGC PAPER 2004-2005_final.doc | JOURNAL OF AIRCRAFT Vol. 41, No. 4, July–August 2004 Dynamics and Control of Shock Motion in a Near-Isentropic Inlet Douglas G. MacMartin∗ California Institute of Technology, Pasadena, California 91125DocID: CwPI - View Document |
| Microsoft Word - VSGC PAPER 2004-2005_final.docDocID: BMPp - View Document |
| National Aeronautics and Space Administration NASA’s Aeronautics Test Program 10- by 10-Foot Supersonic Wind TunnelDocID: fsXg - View Document |
| National Aeronautics and Space Administration NASA’s Aeronautics Test Program 10- by 10-Foot Supersonic Wind TunnelDocID: fnLr - View Document |
| Council of Scientific and Industrial Research National Aerospace Laboratories Experimental Aerodynamics CSIR-NALDocID: 9NIX - View Document |