Supersonic aeroelastic applications of harmonic potential panel method to oscillating flexible bodies
- 1 July 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 25 (4) , 271-277
- https://doi.org/10.2514/3.25999
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- A harmonic gradient method for unsteady supersonic flow calculationsJournal of Aircraft, 1985
- Numerical simulation of steady supersonic flow over an ogive-cylinder-boattail bodyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Reynolds number criticality in dynamic testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Calculation of Unsteady Subsonic Flow about Harmonically Oscillating Wing/Body ConfigurationsJournal of Aircraft, 1977
- Dynamic stability analysis of bodies of revolution in supersonic flow.Journal of Spacecraft and Rockets, 1968
- Aeroelastic instability caused by slender payloads.Journal of Spacecraft and Rockets, 1967
- Analysis of flow separation effects on the dynamics of a large space boosterJournal of Spacecraft and Rockets, 1965
- Second-Order Theory for Unsteady Supersonic Flow Past Slender, Pointed Bodies of RevolutionJournal of the Aerospace Sciences, 1960
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- First- and Second-Order Theory of Supersonic Flow Past Bodies of RevolutionJournal of the Aeronautical Sciences, 1951