Incoming Resources
- Interactive calculation procedures for mixed compression inlets, Eli Reshotko
- Experimental investigation of the application of microramp flow control to an oblique shock interaction, Stefanie M. Hirt and Bernhard H. Anderson ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
- Convection of a pattern of vorticity through a reacting shock wave, T.L. Jackson, A.K. Kapila, M.Y. Hussaini
- Matched asymptotic expansions to similarity solutions of shock diffraction, Eduard Harabetian
- Interaction of minor ions with fast and slow shocks, final report, Y.C. Whang
- Measured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet, Domenic J. Maglieri and Herbert R. Henderson, Ana F. Tinetti
- Final report for NASA grant NAG 5-844
- Computational modeling and validation for hypersonic inlets, Louis A. Povinelli ; prepared for the 75th Symposium on Hypersonic Combined Cycle Propulsion sponsored by the Propulsion and Energetics Panel of AGARD, Madrid, Spain, May 28-June 1, 1990
- Statistical analysis of a large sample size pyroshock test data set including post flight data assessment, James William O. Hughes and Anne M. McNelis ; prepared for the 80th Shock and Vibration Symposium sponsored by the Shock and Vibration Information Analysis Center (SAVIAC), San Diego, California, October 25-29, 2009
- Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields, Gary E. Erickson
- Some notes on shock resolving flux functions, Timothy J. Barth, Part 1
- Flow separation in shock wave boundary layer interactions at hypersonic speeds, A. Hamed
- Optical techniques for determination of normal shock position in supersonic flows for aerospace applications, Grigory Adamovsky and John G. Eustace ; prepared for the Conference on Optical Testing and Metrology III sponsored by the Society of Photo-Optical Instrumentation Engineers, San Diego, California, July 8-13, 1990
- Assessment of computational fluid dynamics (CFD) models for shock boundary-layer interaction, James R. DeBonis [and others] ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28 to July 1, 2010
- Extending post-processing and run time capabilities of the CTH shock physics code, Jerry A. Clarke and Eric R. Mark
- Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks, Jan Lepicovsky, Timothy J. Bencic
- Jet noise reduction by microjets, a parametric study, K.B.M.Q. Zaman ; prepared for the 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) cosponsored by AIAA and CEAS, Miami, Florida, May 11-13, 2009
- Direct visualization of shock waves in supersonic space shuttle flight, J.M. O'Farrell, T.J. Rieckhoff
- Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry, Gregory C. Herring and James F. Meyers
- Broadband shock noise in internally-mixed dual-stream jets, James E. Bridges ; prepared for the 15th Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) cosponsored by AIAA and CEAS, Miami, Florida, May 11-13, 2009
- A study of fundamental shock noise mechanisms, Kristine R. Meadows