Preliminary design of composite wings for buckling, strength and displacement constraints-Reference-Cited by-同舟云学术

Preliminary design of composite wings for buckling, strength and displacement constraints

Published:1978-04-03 Issue: Volume: Page:
ISSN:
Container-title:19th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

STARNES, JR. J.¹,HAFTKA R.²

Affiliation:

1. NASA, Langley Research Center, Structures and Dynamics Div., Hampton, Va.

2. Illinois Institute of Technology, Chicago, Ill.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1978-466

Reference13 articles.

1. Schnit,L. A,Jr. ,and hamaLathm,R. K. "A WtUevel Approach for Minimum Weight Structural Decign Includirig lacel -6 System Buckling Constraints," AAIkA Paper Ro. 77-373, 3.977

2. Haf'tka, Haphael T."utomatedProcedure f@r Design of Wing Structures tc Satisfy Strengtk and Flutter Requirements,"TN c-& 1973, nE:

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