Gautam et al., 2017 - Google Patents
Experimental study of supersonic flow over cavity with aft wall offset and cavity floor injectionGautam et al., 2017
- Document ID
- 8776200745042884827
- Author
- Gautam T
- Lovejeet G
- Vaidyanathan A
- Publication year
- Publication venue
- Aerospace Science and Technology
External Links
Snippet
Experimental studies were conducted at Mach 1.71 supersonic flow over open cavity to find the best configuration of combined passive (aft wall offset) and active methods (cavity floor injection) to optimize the noise suppression. Cavity of length to depth ratio 3 with 0%, 5 …
- 238000002347 injection 0 title abstract description 97
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