Unsteady supersonic flow calculations for wing-body combinations using harmonic gradient method
- 1 April 1990
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (4) , 635-641
- https://doi.org/10.2514/3.10440
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Analysis of unsteady aerodynamics for elastic bodies in supersonic flowJournal of Aircraft, 1987
- 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
- 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
- The Supersonic Triplet-A New Aerodynamic Panel Singularity with Directional PropertiesAIAA Journal, 1980
- Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex ConfigurationsAIAA Journal, 1975
- Linearized characteristics method for supersonic flow past vibratingshells.AIAA Journal, 1973
- Analysis and design of wing-body combinations at subsonic and supersonic speeds.Journal of Aircraft, 1968