Subsonic Transport Composite Wing Model for Optimization Studies-Reference-Cited by-同舟云学术

Subsonic Transport Composite Wing Model for Optimization Studies

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
Short-container-title:

Author:

Albers Robert¹,Tuttle Mark¹,Avery William²

Affiliation:

1. University of Washington

2. Boeing Commercial Airplanes

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6016

Reference36 articles.

1. Design of minimum mass structures with specified natural frequencies.

2. 2Dwyer, W. J., Emerton R. K., and Sabatelli P. L. "An Automated Procedure for the Optimization of Practical Aerospace Structures, Vol.II: Programmer's Manual", Air Force Flight Dynamics Laboratory, Report AFFDL-TR-70-118, Wright-Patterson AFB,OH,Apr., 1971.

3. 3Lynch,R.W.,RogersW.A.,BraymanW.W.,andHertzT.J."AeroelasticTailoringofAdvancedCompositeStructuresfor Military Aircraft, Vol.III: Modifications and User's Guide for Procedure TSO", Air Force Flight Dynamics Laboratory, Report AFFDL-TR-76-100, Wright-PattersonAFB, OH,April, 1971. Wright-Patterson AFB,OH, Feb., 1978.

4. 4Markowitz, J., and Isakson G. "FASTOP-3: A Strength, Deflection, and Flutter Optimization Program for Metallic and Composite Structures, Vol.I: Theory and Application", Air Force Flight Dynamics Laboratory, Report AFFDL-TR-78-50, Wright-PattersonAFB,OH, May,1978.

5. 5Markowitz, J., and Isakson G. "FASTOP-3: A Strength, Deflection, and Flutter Optimization Program for Metallic and Composite Structures, Vol.II: Program User's Guide", Air Force Flight Dynamics Laboratory, Report AFFDL-TR-78-50, Wright-PattersonAFB,OH, May,1978.