Transition effects on slender cone pitch damping
- 1 January 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 25 (1) , 4-8
- https://doi.org/10.2514/3.25980
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Coupling between vehicle motion and slender cone transitionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Effects of Flow Separation on Shuttle Longitudinal Dynamics and Aeroelastic StabilityJournal of Spacecraft and Rockets, 1977
- Generalized unsteady embedded Newtonian flowJournal of Spacecraft and Rockets, 1975
- Unsteady Aerodynamics of Slender Delta Wings at Large Angles of AttackJournal of Aircraft, 1975
- Correlation of Attitude Effects on Slender Vehicle TransitionAIAA Journal, 1974
- Transition Effects on Slender Vehicle Stability and Trim CharacteristicsJournal of Spacecraft and Rockets, 1974
- Unsteady Airfoil Stall, Review and ExtensionJournal of Aircraft, 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
- Analysis of flow separation effects on the dynamics of a large space boosterJournal of Spacecraft and Rockets, 1965