Loose Fluid-Structure Coupled Approach for a Rotor in Descent Incorporating Fuselage Effects-Reference-Cited by-同舟云学术

Loose Fluid-Structure Coupled Approach for a Rotor in Descent Incorporating Fuselage Effects

Published:2013-07 Issue:4 Volume:50 Page:1016-1026
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Jung Sung Nam¹,Sa Jeong Hwan¹,You Young Hyun¹,Park Jae Sang¹,Park Soo Hyung¹

Affiliation:

1. Department of Aerospace Information Engineering, Konkuk University, Seoul 143-701, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031826

Reference13 articles.

1. van der WallB. G. “2nd HHC Aeroacoustic Rotor Test (HART II), Part I: Test Documentation,” DLR, German Aerospace Research Center Inst. Rept. IB-111-2003/31, Brunswick, Germany, 2003.

2. van der WallB. G.BurleyC. L. “2nd HHC Aeroacoustic Rotor Test (HART II), Part II: Representative Results,” DLR, German Aerospace Research Center Inst. Rept. IB-111-2005/03, Brunswick, Germany, 2005.

3. Prediction of Rotor Structural Loads with Comprehensive Analysis

4. Calculation of Rotor Blade-Vortex Interaction Airloads Using a Multiple-Trailer Free-Wake Model

5. Correlation of Aeroelastic Response and Structural Loads for a Rotor in Descent

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