NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Experimental creep data for a built-up aluminum/titanium structure subjected to heating and loadingExperimental creep, temperature, and strain data resulting from a laboratory experiment on a built-up aluminum/titanium structure are presented. The structure and the experiment are described in detail. A heating and loading experiment lasting approximately six hours is conducted on a test structure. Considerable creep strain resulted from compressive stresses in the heated skin. Large residual stresses were found after the experiment was completed. The residual stresses in the substructure frames were large enough to preclude further cycles of creep experiments with this built-up structure because of concern that the frame webs would buckle.
Document ID
19830014358
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jenkins, J. M.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Montoya, C. A.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-84906
NAS 1.15:84906
Report Number: NASA-TM-84906
Report Number: NAS 1.15:84906
Accession Number
83N22629
Funding Number(s)
PROJECT: RTOP 506-53-64
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available