Validation of an unstructured grid Euler/Navier-Stokes code on a full aircraft with propellers

Author:

Goble B.1,Hooker J.1

Affiliation:

1. Lockheed Martin Aeronautics Co., Marietta, GA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Comparison of Multi-Fidelity Prediction Methods for an Integrated Propeller;AIAA AVIATION 2021 FORUM;2021-07-28

2. Application of the HPCMP CREATETM-AV Kestrel to the 1st AIAA Workshop for Integrated Propeller Prediction;AIAA AVIATION 2020 FORUM;2020-06-08

3. Aeroelastic Analysis for the High Altitude Propeller by Using Fluid-Structure Interaction Method;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2018

4. Time-Accurate Simulations of a Spinning Propeller Using OVERFLOW2;32nd AIAA Applied Aerodynamics Conference;2014-06-13

5. Over Wing Nacelle Installations for Improved Energy Efficiency;31st AIAA Applied Aerodynamics Conference;2013-06-22

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