Optimal Shape Design of Mail-Slot Nacelle on N3-X Hybrid Wing Body Configuration-Reference-Cited by-同舟云学术

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Optimal Shape Design of Mail-Slot Nacelle on N3-X Hybrid Wing Body Configuration

Published:2013-06-22 Issue: Volume: Page:
ISSN:
Container-title:31st AIAA Applied Aerodynamics Conference
language:
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Author:

Kim Hyoungjin¹,Liou Meng-Sing²

Affiliation:

1. SAIC

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2413

Reference30 articles.

1. 2Liebeck,R.H.DesignoftheBlendedWingBodySubsonicTransport,‖J.Aircraft,Vol.41,No.1,2004.

2. Airframe Design for Silent Fuel-Efficient Aircraft

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3. Development of a coupled supersonic inlet-fan Navier–Stokes simulation method;Chinese Journal of Aeronautics;2018-02

4. Mail-Slot Nacelle Shape Design for N3-X Hybrid Wing-Body Configuration;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

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