The unsteady suction analogy and applications
- 17 August 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Effect of Angle of Attack and Mach Number on Slender-Wing Unsteady AerodynamicsJournal of Aircraft, 1978
- Unsteady Aerodynamics of Slender Delta Wings at Large Angles of AttackJournal of Aircraft, 1975
- Effects of Leading-Edge Vortex Flow on the Roll Damping of Slender WingsJournal of Aircraft, 1971
- Application of oscillatory aerodynamic theory to estimation of dynamic stability derivativesJournal of Aircraft, 1970