Comparison of propeller cruise noise data taken in the NASA Lewis 8-by 6-foot wind tunnel with other tunnel and flight data
- 10 April 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Measured noise of a scale model high speed propeller at simulated takeoff/approach conditionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- The development and calibration of an acoustic wall transonic test sectionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Why credible propeller noise measurements are possible in the acoustically untreated NASA Lewis 8 ft by 6 ft wind tunnelThe Journal of the Acoustical Society of America, 1984
- Sound Diffraction by Rigid Spheres and Circular CylindersThe Journal of the Acoustical Society of America, 1947