Impact of Droop and Scarf on the Aerodynamic Performance of Compact Aero-Engine Nacelles-Reference-Cited by-同舟云学术

Impact of Droop and Scarf on the Aerodynamic Performance of Compact Aero-Engine Nacelles

Published:2020-01-05 Issue: Volume: Page:
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Container-title:AIAA Scitech 2020 Forum
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Author:

Tejero Fernando¹,MacManus David¹,Sheaf Christopher²

Affiliation:

1. Cranfield University

2. Rolls-Royce Group plc

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. European Commission, “Flightpath 2050: Europe~s Vision for Aviation,” Tech. Rep. ISBN 978-92-79-19724-6, Publications Office of theEuropean Union, 2011.

2. Optimum Fan Pressure Ratio for Bypass Engines with Separate or Mixed Exhaust Streams

3. Daggett, D. “Ultra-Efficient Engine Technology Systems Integration and Environmental Assessment,” Tech. Rep. CR-2002-211754, NASA, 2002.

4. Effects of Aircraft Integration on Compact Nacelle Aerodynamics

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