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Applications of structural optimization methods to fixed-wing aircraft and spacecraft in the 1980sThis report is the summary of a technical survey on the applications of structural optimization in the U.S. aerospace industry through the 1980s. Since applications to rotary wing aircraft will be covered by other literature, applications to fixed-wing aircraft and spacecraft were considered. It became clear that very significant progress has been made during this decade, indicating this technology is about to become one of the practical tools in computer aided structural design.
Document ID
19930023023
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Miura, Hirokazu (NASA Ames Research Center Moffett Field, CA, United States)
Neill, Douglas J. (Northrop Corp. Hawthorne, CA., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
A-92099
NAS 1.15:103939
NASA-TM-103939
Accession Number
93N32212
Funding Number(s)
PROJECT: RTOP 505-69-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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