2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response-Reference-Cited by-同舟云学术

2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response

Published:1993 Issue: Volume: Page:213-230
ISSN:
Container-title:Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers
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Author:

Holmes D. G.,Chuang H. A.

Publisher

Springer New York

Link

http://link.springer.com/content/pdf/10.1007/978-1-4613-9341-2_11.pdf

Reference20 articles.

1. J. T. Batina. Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshes. AIAA Paper 90–0936, 1990.

2. A. Bolcs and T. H. Fransson. Aeroelasticity in turbomachines: Comparison of theoretical and experimental cascade results. Communication du Laboratoire de Thermique Appliquée et de Turbomachines Nr. 13, L’École Polytechnique Fédérale de Lausanne, 1986.

3. G. Dahlquist and A. Bjorck. Numerical Methods Prentice-Hall, New Jersey, 1974.

4. M. B. Giles. UNSFLO: A numerical method for unsteady in-viscid flow in turbomachinery. Computational Fluid Dynamics Laboratory Report CFDL-TR-86–6, MIT, 1986.

5. M. B. Giles. Non-reflecting boundary conditions for the Euler equations. Computational Fluid Dynamics Laboratory Report CFDL-TR-88–1, MIT, 1988.

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