Aerodynamic Analysis of Civil Aeroengine Exhaust Systems Using Computational Fluid Dynamics
Author:
Affiliation:
1. Cranfield University, Bedford, England MK43 0AL, United Kingdom
2. Rolls–Royce plc., Derby, England DE24 8BJ, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Rolls-Royce plc.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36867
Reference42 articles.
1. Optimum Fan Pressure Ratio for Bypass Engines with Separate or Mixed Exhaust Streams
2. Aerodynamic Design of Separate-Jet Exhausts for Future Civil Aero-engines—Part I: Parametric Geometry Definition and Computational Fluid Dynamics Approach
3. Elements of Propulsion: Gas Turbines and Rockets
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