ASTROP2-LE - A flutter and forced response analysis system based on a 2D linearized Euler solver-Reference-Cited by-同舟云学术

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ASTROP2-LE - A flutter and forced response analysis system based on a 2D linearized Euler solver

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Reddy T.¹,Srivastava R.¹,Mehmed O.²

Affiliation:

1. Toledo, Univ., OH

2. NASA, Glenn Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2679

Reference30 articles.

1. (l)Reddy, et al, "A review of Recent Aeroelastic Analysis Methods for Propulsion at NASA Lewis IResearchCenter0022,NASA TP 3406,December1993.

2. (S)Rao,B. M. and Jones,W. P. "Unsteady Airloads on a Cascadeof Staggered Blades in Subsonic Flow0022, PaperNo. 32, AGARD-CP-177, September1975.

3. Unsteady Flow in a Supersonic Cascade with Subsonic Leading-Edge Locus

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