An Output-Based Adaptive and Higher-Order Method for a Rotor in Hover-Reference-Cited by-同舟云学术

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An Output-Based Adaptive and Higher-Order Method for a Rotor in Hover

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:26th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Modisette James¹,Darmofal David¹

Affiliation:

1. Massachusetts Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-7343

Reference42 articles.

1. 4O'Brien, D. M., Analysis of Computational Modeling Techniques for Complete Rotorcraft Configurations, Ph.D. thesis,Georgia Institute of Technology, Atlanta, Georgia, 2006.

2. Flowfield Analysis of Modern Helicopter Rotors in Hover by Navier‐Stokes Method

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