Design optimization of satellite structures for frequency, strength,and buckling requirements-Reference-Cited by-同舟云学术

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Design optimization of satellite structures for frequency, strength,and buckling requirements

Published:1993-01-11 Issue: Volume: Page:
ISSN:
Container-title:31st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

KODIYALAM SRINIVAS¹,GRAICHEN CATHERINE¹,CONNELL ISOBEL¹,FINNIGAN PETER¹

Affiliation:

1. GE Solid Mechanics Lab., Schenectady, NY

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-98

Reference14 articles.

1. [I]Viinderplaats. G.N.,Nione,ical Opriniizarioii Techniqiresfor EigineeiingDesign:wirh Applicatiomr,McGraw-Hill, New York, 1984.

2. [2]Viintlerplaats,G.N.,ADSUser'sMailrial,VMAEngineering, CaIifi)rnia,March 1988.

3. 141Sohicski,J."Optimizationby Decomposition:A Stcpfrom IlierarchictoNon-I-licrarchic Systems,"Recenl Advatice.r irMir/lirliscip/iiia!y Ajialy.i.smid Oprimizulion, NASA (F3031, 1988.

4. IS] Rruhn, E.E,Atialyrisand Design ofP/i& VeiicleSmrctirres, Jacobs Publishing, Inc., U.S.A.,1973.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Engineering Applications of Satellite Structural Optimization Utilizing ANSYS/CATIA;Applied Mechanics and Materials;2011-10-24

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