Aeroelastic Analysis of Helicopter Rotor Blades on Deformable Chimera Grids-Reference-Cited by-同舟云学术

Aeroelastic Analysis of Helicopter Rotor Blades on Deformable Chimera Grids

Published:2004-05 Issue:3 Volume:41 Page:577-584
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Pomin Hubert¹,Wagner Siegfried¹

Affiliation:

1. University of Stuttgart, D-70550 Stuttgart, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.11484

Reference26 articles.

1. Flow Phenomena on Rotary Wing Systems and their Modeling

2. 2Krämer, E. "Theoretische Untersuchungen der stationären Rotorblattumströmung mit Hilfe eines Euler-Verfahrens," Ph.D. Dissertation, Univ. of the German Army, Inst. for Aeronautics and Aircraft Structures, Fortschritt-Berichte VDI, Reihe 7,Munich, No. 197, July 1991.

3. 4Stangl, R. "Ein Euler-Verfahren zur Berechnung der Strömung um einen Hubschrauber im Vorwärtsflug," Ph.D. Dissertation,Univ. of Stuttgart, Inst. of Aerodynamics and Gas Dynamics, Stuttgart, Germany,Oct.1996.

4. Evaluation of a Navier‐Stokes Analysis Method for Hover Performance Prediction

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