Oscillating wings and bodies with flexure in supersonic flow
- 1 June 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (6) , 507-514
- https://doi.org/10.2514/3.45614
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- A harmonic gradient method for unsteady supersonic flow calculationsJournal of Aircraft, 1985
- Doublet-Point Method for Supersonic Unsteady Lifting Surfaces.AIAA Journal, 1984
- Improved Potential Gradient Method to Calculate Airloads on Oscillating Supersonic Interfering SurfacesJournal of Aircraft, 1982
- Viscous Effects on Missile Aerodynamics at Low Angles of AttackJournal of Spacecraft and Rockets, 1981
- An Improved Mach-Box Approach for Supersonic Oscillatory PressuresJournal of Aircraft, 1977
- Higher approximations for supersonic flow past slowly oscillating bodies of revolutionActa Mechanica, 1968
- On supersonic flow past oscillating bodies of revolution.AIAA Journal, 1966
- StructuresJournal of the Royal Aeronautical Society, 1956
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951
- Resistance of Slender Bodies Moving With Supersonic Velocities, With Special Reference to ProjectilesTransactions of the American Society of Mechanical Engineers, 1932