A model for slat noise generation
- 12 May 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Emendation of the Brown & Michael equation, with application to sound generation by vortex motion near a half-planeJournal of Fluid Mechanics, 1996
- An example of active circulation control of the unsteady separated flow past a semi-infinite plateJournal of Fluid Mechanics, 1994
- Panel Methods in Computational Fluid DynamicsAnnual Review of Fluid Mechanics, 1990
- The influence of surface rounding on trailing edge noiseJournal of Sound and Vibration, 1988
- The influence of vortex shedding on the generation of sound by convected turbulenceJournal of Fluid Mechanics, 1976
- High-Lift AerodynamicsJournal of Aircraft, 1975
- An inviscid model of two-dimensional vortex sheddingJournal of Fluid Mechanics, 1973
- Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half planeJournal of Fluid Mechanics, 1970
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968
- A theory of the flow past a slender delta wing with leading edge separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959