Parameter Sensitivity Analysis and Rapid Performance Calculation for High Bypass Ratio Separate Flow Exhaust System
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_39
Reference16 articles.
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3. Keith BD, Uenishi K, Dietrich DA (1991) CFD-based 3D turbofan nozzle analysis system. In: AIAA/SAE/ASME 27th joint propulsion conference, Sacramento, CA, 24–26 June 1991
4. Peery KM, Forester CK (1979) Numerical simulation of multistream nozzle flow. AIAA-79-1549
5. Norton RJG, Kingsley JP (1992) Rolls-Royce Inc. prediction of a high bypass ratio engine exhaust nozzle flowfield. AIAA-92-3259
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