Model and full scale test results relating to fan noise in-flight effects
- 24 March 1975
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Effects of forward velocity and acoustic treatment on inlet fan noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Sources of unsteady flow in subsonic aircraft inletsThe Journal of the Acoustical Society of America, 1974