Supersonic vehicle research addresses the development of tools, technologies, and knowledge to help eliminate technical barriers to practical commercial supersonic flight. While the major focus of this research has been on reducing the ground signature at supersonic cruise, airplanes must also satisfy noise constraints during takeoff and landing at subsonic speeds, and jet noise is the main sound source. We use computational aeroacoustic sim- ulation tools to assess new designs at these lower speeds. We are further scrutinizing both modeling and simulation practices and the use of hybrid Reynolds-averaged Navier Stokes/Large- Eddy Simulations methods and developing new methods to predict jet noise on a full flight configuration.
Predicting Jet Noise for Full-Scale Low-Boom Aircraft
International Conference for High Performance Computing, Networking, Storage, and Analysis ; 2019 ; Denver, CA, United States
2019-11-17
Conference paper
No indication
English
Aircraft Engine Noise and Sonic Boom
NTIS | 1970
|Aircraft Engine Noise and Sonic Boom
NTIS | 1969
Aircraft Engine Noise and Sonic Boom
NTIS | 1969
Aircraft Engine Noise and Sonic Boom
NTIS | 1969
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NTRS | 1968