Viscous Effects on Missile Aerodynamics at Low Angles of Attack
- 1 September 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 18 (5) , 401-405
- https://doi.org/10.2514/3.57834
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Effect of Mach Number on Slender Vehicle DynamicsJournal of Spacecraft and Rockets, 1981
- Transonic Sting InterferenceJournal of Spacecraft and Rockets, 1980
- Vortex-induced asymmetric loads in 2-D and 3-D flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Reynolds number criticality in dynamic testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Correlation of Attitude Effects on Slender Vehicle TransitionAIAA Journal, 1974
- Transition Effects on Slender Vehicle Stability and Trim CharacteristicsJournal of Spacecraft and Rockets, 1974
- Dynamic Stability Tests of Spinning Entry Bodies in the Terminal RegimeJournal of Spacecraft and Rockets, 1971
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969
- Aeroelastic instability caused by slender payloads.Journal of Spacecraft and Rockets, 1967
- FREE FLIGHT MOTION OF SYMMETRIC MISSILESPublished by Defense Technical Information Center (DTIC) ,1963