Effect of Angle of Attack and Mach Number on Slender-Wing Unsteady Aerodynamics
- 1 June 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (6) , 358-365
- https://doi.org/10.2514/3.58370
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Approximate Nonlinear Slender Wing AerodynamicsJournal of Aircraft, 1977
- Effects of Flow Separation on Shuttle Longitudinal Dynamics and Aeroelastic StabilityJournal of Spacecraft and Rockets, 1977
- Errata: Unsteady Aerodynamics of Slender Delta Wings at Large Angles of AttackJournal of Aircraft, 1977
- Unsteady Aerodynamics of Slender Delta Wings at Large Angles of AttackJournal of Aircraft, 1975
- Dynamic Support InterferenceJournal of Spacecraft and Rockets, 1972
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Boundary-layer transition and dynamic sting interferenceAIAA Journal, 1970