Negatively scarfed inlets for acoustic reduction, aerodynamic performance assessment-Reference-Cited by-同舟云学术

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Negatively scarfed inlets for acoustic reduction, aerodynamic performance assessment

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Nangia R.¹,Palmer M.¹

Affiliation:

1. Nangia Aero Research Associates, Bristol, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-354

Reference9 articles.

1. Fonun "Aspecg ok Engine / Airfiake Inte&ation0022, March 1999,Pau,Fxance.

2. NANGL4, R.K., PALMER, ME. & HODGES, J. "Modelling of 3-D Aircraft Inletsat ero'Speed(& Low Speeds with Cross-Wind) & Flow Separation Prediction0022,RAeS- IMechE Conference"Verification of DesignMethods by Test & Analysis0022, November 1998, London, UK.

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2. Impact of Droop and Scarf on the Aerodynamic Performance of Compact Aero-Engine Nacelles;AIAA Scitech 2020 Forum;2020-01-05

3. Surrogate-Based Aerodynamic Shape Optimization of a Civil Aircraft Engine Nacelle;AIAA Journal;2007-10

4. Inlets with negative scarf for acoustic reduction - Aerodynamic assessment at transonic speed;18th Applied Aerodynamics Conference;2000-08-14

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