Aerodynamic Effects of Propulsion Integration for High Bypass Ratio Engines
Author:
Affiliation:
1. Cranfield University, Cranfield MK43 0AL, England, United Kingdom
2. Rolls-Royce, plc., Derby DE24 8BJ, England, United Kingdom
Funder
Rolls Royce
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034150
Reference33 articles.
1. DalyM. (ed.), Jane’s Aero-Engines, 28th ed., IHS Global, Ltd., Surrey, England, U.K., 2010, pp. 28–30.
2. Aerodynamic aspects of engine-aircraft integration of transport aircraft
3. Computation of Engine-Airframe Installation Drag
4. A Correct Thrust Determination Method for Turbine Powered Simulators in Wind Tunnel Testing
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