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Experimental investigation of thermal-buckling characteristics of flanged, thin-shell leading edgesThermal buckling characteristics of flanged thin shell leading edges - aerodynamic heating
Document ID
19660006204
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jenkins, J. M.
(NASA Flight Research Center Edwards, CA, United States)
Sefic, W. J.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3243
Report Number: NASA-TN-D-3243
Accession Number
66N15493
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LEADING EDGE
THERMAL BUCKLING
THIN WALLED SHELL
AERODYNAMIC HEATING
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