Aerodynamics, Hypersonic
Label
Aerodynamics, Hypersonic
Name
Aerodynamics, Hypersonic
Actions
Incoming Resources
- Subject of21
- Application of computational fluid dynamics in high speed aeropropulsion, Louis A. Povinelli
- On the instability of hypersonic flow past a flat plate, Nicholas Blackaby, Stephen Cowley, Philip Hall
- SRM-assisted trajectory for the GTX reference vehicle, John Riehl and Charles Trefny, Daniel Kosareo
- Final report on NASA grant no. NAG-1-1029, optimization and guidance of flight trajectories for the national aerospace plane, by A. Miele
- Development of a high accuracy angular measurement system for Langley Research Center hypersonic wind tunnel facilities, Brett Newman and Si-bok Yu
- The study of pressure measurement techniques and devices in the range of 10[exp-1] to 10[exp-5] torr (2 millipsi to 0.2 micropsi), final technical report, by Dr. John H. Hoffman
- NESC review of the 8-Foot High Temperature Tunnel (HTT) oxygen storage pressure vessel inspection requirements, Michael Gilbert [and others]
- Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees, Ramadas K. Prabhu
- 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
- Separation characteristics of generic stores from lee side of an inclined flat plate at Mach 6, Floyd J. Wilcox, Jr
- CFD for hypersonic propulsion, Louis A. Povinelli
- Comparison of nonequilibrium solution algorithms applied to chemically stiff hypersonic flows, G. Palmer and E. Venkatapathy
- Current capabilities and future directions in computational fluid dynamics, Committee to Assess Current Capabilities and Future Directions in Computational Fluid Dynamics, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council
- Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition, Rudolph A. King, Scott A. Berry, Michael A. Kegerise
- Control activity in support of NASA Turbine Based Combined Cycle (TBCC) research, Thomas J. Stueber [and others]
- Flow separation in shock wave boundary layer interactions at hypersonic speeds, A. Hamed
- Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows, progress report for the period ended December 31, 1989, by D. J. Singh and S. N. Tiwari ; prepared for National Aeronautics and Space Administration, Langley Research Center
- Transpiration cooling in hypersonic flight, Domingo Tavelia and Leonard Roberts
- Multidisciplinary analysis of a hypersonic engine, M.E.M. Stewart [and others] ; prepared for the 11th International Conference on Space Planes and Hypersonic Systems and Technologies ... September 29-October 4, 2002
- Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition, John W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field, Scott D. Holland
Outgoing Resources
- Focus1