NASA NTRS · 20010080469
Flow Solution for Advanced Separate Flow Nozzles Response A: Structured Grid Navier-Stokes Approach
Abstract
NASA Glenn Research Center funded a computational study to investigate the effect of chevrons and tabs on the exhaust plume from separate flow nozzles. Numerical studies were conducted at typical takeoff power with 0.28 M flight speed. Report provides numerical data and insights into the mechanisms responsible for increased mixing.
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Kenzakowski, D. C., Shipman, J., Dash, S. M., Saiyed, Naseem. 2001-04-01. Flow Solution for Advanced Separate Flow Nozzles Response A: Structured Grid Navier-Stokes Approach. https://ntrs.nasa.gov/citations/20010080469
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