Aeroacoustic measurements of slat noise on a three-dimensional high-lift system
- 10 May 1999
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Reynolds averaged Navier-Stokes computations of a flap side-edge flow fieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Aeroacoustic measurements of a wing-flap configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Computations of viscous flows for multi-element wings using hybrid structured-unstructured gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Phased arrays for aeroacoustic testing - Theoretical developmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- A comparison of turbulence models in computing multi-element airfoil flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Noise generation by a lifting wing/flap combination at Reynolds numbers to 2.8 x 10 to the 6thPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Airframe noise component interaction studiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Measurements of noise produced by flow past lifting surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978