Helicopter Rotor Design Using a Time-Spectral and Adjoint-Based Method-Reference-Cited by-同舟云学术

Helicopter Rotor Design Using a Time-Spectral and Adjoint-Based Method

Published:2014-03 Issue:2 Volume:51 Page:412-423
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Choi Seongim¹,Lee Kihwan¹,Potsdam Mark M.²,Alonso Juan J.¹

Affiliation:

1. Department of Aeronautics and Astronautics, Stanford University, Stanford, California 94305

2. U.S. Army Aviation Development Directorate—Aeroflightdynamics Directorate (AMRDEC) Research, Development, and Engineering Command, Moffett, California 94305

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031975

Reference28 articles.

1. also AIAA Paper 1998-4733.

2. CanutoC.HussainiM. Y.QuarteroniA.ZangT. A.Jr., Spectral Methods in Fluid Dynamics, Springer Series in Computational Physics, Springer–Verlag, New York, 1998, pp. 32–45.

3. Fourier spectral methods

4. The computational efficiency of non-linear frequency domain methods

5. also AIAA Paper 2006-0445.

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