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Astronautic Structures Manual, Volume 3This document (Volumes I, II, and III) presents a compilation of industry-wide methods in aerospace strength analysis that can be carried out by hand, that are general enough in scope to cover most structures encountered, and that are sophisticated enough to give accurate estimates of the actual strength expected. It provides analysis techniques for the elastic and inelastic stress ranges. It serves not only as a catalog of methods not usually available, but also as a reference source for the background of the methods themselves. An overview of the manual is as follows: Section A is a general introduction of methods used and includes sections on loads, combined stresses, and interaction curves; Section B is devoted to methods of strength analysis; Section C is devoted to the topic of structural stability; Section D is on thermal stresses; Section E is on fatigue and fracture mechanics; Section F is on composites; Section G is on rotating machinery; and Section H is on statistics. These three volumes supersede Volumes I and II, NASA TM X-60041 and NASA TM X-60042, respectively.
Document ID
19760071127
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-73307
NASA-TM-X-60041
NASA-TM-X-60042
Accession Number
76N76168
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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