NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Methods for structural design at elevated temperaturesA procedure which can be used to design elevated temperature structures is discussed. The desired goal is to have the same confidence in the structural integrity at elevated temperature as the factor of safety gives on mechanical loads at room temperature. Methods of design and analysis for creep, creep rupture, and creep buckling are presented. Example problems are included to illustrate the analytical methods. Creep data for some common structural materials are presented. Appendix B is description, user's manual, and listing for the creep analysis program. The program predicts time to a given creep or to creep rupture for a material subjected to a specified stress-temperature-time spectrum. Fatigue at elevated temperature is discussed. Methods of analysis for high stress-low cycle fatigue, fatigue below the creep range, and fatigue in the creep range are included. The interaction of thermal fatigue and mechanical loads is considered, and a detailed approach to fatigue analysis is given for structures operating below the creep range.
Document ID
19730014124
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ellison, A. M.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Jones, W. E., Jr.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Leimbach, K. R.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
LMSC/HREC-D306579
NASA-CR-124232
HREC-8170-1
Report Number: LMSC/HREC-D306579
Report Number: NASA-CR-124232
Report Number: HREC-8170-1
Accession Number
73N22851
Funding Number(s)
CONTRACT_GRANT: NAS8-28170
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available