AN IMPROVED MACH-BOX APPROACH FOR THE CALCULATION OF SUPERSONIC OSCILLATORY PRESSURE DISTRIBUTIONS
- 5 May 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Oscillatory supersonic lifting surface theory using a finite elementdoublet representationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- The supersonic doublet-lattice method - A comparison of two approachesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Theoretical studies to refine the prediction of unsteady aerodynamics of supersonic elastic aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- FURTHER DEVELOPMENTS IN SUPERSONIC AERODYNAMIC INFLUENCE COEFFICIENT METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- A Study of Surge in Compressors and Jet EnginesJournal of the Aeronautical Sciences, 1955