Derivation of Aerodynamic Kernel Functions
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (11) , 1586-1588
- https://doi.org/10.2514/3.50642
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- On numerical methods to impose asymptotic boundary conditions of boundary-layer equationsComputers & Fluids, 1974
- Numerical stability of boundary layers with massive blowing.AIAA Journal, 1973
- Fluctuating lift and moment coefficients for cascaded airfoils in a nonuniform compressible flow.Journal of Aircraft, 1973
- Solution of Unsteady Flow of Power Law FluidsAIAA Journal, 1972
- On laminar boundary-layer blow-off. Part 2Journal of Fluid Mechanics, 1971
- Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutterAIAA Journal, 1971
- Numerical solution of boundary-layer flows with massive blowingAIAA Journal, 1971
- Flame Sheet Model for Stagnation Point FlowsCombustion Science and Technology, 1971
- Numerical analysis of stagnation point flows with massive blowingAIAA Journal, 1970
- The Compressible Flow Past an Oscillating Airfoil in a Wind TunnelJournal of the Aeronautical Sciences, 1956