Further studies of harmonic gradient method for supersonic aeroelastic applications
- 1 September 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (9) , 598-605
- https://doi.org/10.2514/3.46070
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Aeroservoelastic wind-tunnel investigations using the active flexible wing model - Status and recent accomplishmentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Supersonic aeroelastic applications of harmonic potential panel method to oscillating flexible bodiesJournal of Spacecraft and Rockets, 1988
- Unsteady supersonic computations of arbitrary wing-body configurations including external storesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Unsteady supersonic flow calculations for wing-body combinations using harmonic gradient methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Constant pressure panel method for supersonic unsteady airload analysisJournal of Aircraft, 1987
- Nonplanar, supersonic, three-dimensional, oscillatory, piecewise continuous-kernel function methodJournal of Aircraft, 1987
- Oscillatory supersonic kernel function method for interfering surfacesJournal of Aircraft, 1974
- Oscillatory Supersonic Kernel Function Method for Isolated WingsJournal of Aircraft, 1974
- Interpolation using surface splines.Journal of Aircraft, 1972
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956