Hypersonic rarefied flow about plates at incidence
- 1 August 1991
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (8) , 1250-1258
- https://doi.org/10.2514/3.10729
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Application of the direct simulation Monte Carlo method to the full shuttle geometryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Fluid dynamic modeling and numerical simulation of low-density hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Orbital acceleration research experimentJournal of Spacecraft and Rockets, 1987
- Direct simulation of aerothermal loads for an aeroassist flight experiment vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Monte Carlo simulation of rarefied flow along a flat platePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Rarefied-flow aerodynamics and thermosphere structure from Shuttle flight measurementsJournal of Spacecraft and Rockets, 1986
- Shuttle Orbiter high resolution accelerometer package experiment - Preliminary flight resultsJournal of Spacecraft and Rockets, 1985
- Rarefied hypersonic flow about cones and flat plates by Monte Carlo simulationAIAA Journal, 1971
- Angle of attack and leading edge effects on the flow about a flat plate at Mach number 18.AIAA Journal, 1968