Transition effects on slender vehicle stability and trim characteristics
- 10 January 1973
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 17 references indexed in Scilit:
- Re-Entrv Camule DynamicsJournal of Spacecraft and Rockets, 1971
- Influence of Asymmetric Transition on Re-Entry Vehicle CharacteristicsJournal of Spacecraft and Rockets, 1971
- A new treatment of roll-pitch coupling for ballistic re-entry vehiclesAIAA Journal, 1970
- Combined effects of mass addition and nose bluntness on boundary-layer transitionAIAA Journal, 1970
- Three-dimensional laminar boundary-layer transition on a sharp 8 degcone at Mach 10AIAA Journal, 1970
- Ballistic range tests of ablating and nonablating slender conesAIAA Journal, 1970
- Universal scaling laws for nose bluntness effects on hypersonic unsteady aerodynamicsAIAA Journal, 1969
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Laminar heat transfer to spherically blunted cones at hypersonic conditionsAIAA Journal, 1964