Comparison of Two Types of Structural Optimization Procedures for Flutter Requirements-Reference-Cited by-同舟云学术

Comparison of Two Types of Structural Optimization Procedures for Flutter Requirements

Published:1975-10 Issue:10 Volume:13 Page:1333-1339
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Haftka Raphael T.¹,Starnes James H.²,Barton Furman W.³,Dixon Sidney C.²

Affiliation:

1. Technion — Israel Institute of Technology, Haifa, Israel

2. NASA Langley Research Center, Hampton, Va.

3. University of Virginia, Charlottesville, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.60545

Reference17 articles.

1. 2Rao, S.S. "Automated Optimum Design of Aircraft Wings to Satisfy Strength, Stability, Frequency, and Flutter Requirements," Ph.D. thesis,Oct. 1971, Division of Solid Mechanics,Structures, and Mechanical Design,Case Western Reserve University, Cleveland, Ohio.

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