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Experimental investigation at mach number 3.0 of the effects of thermal stress and buckling on the flutter of four bay aluminium alloy panels with length width ratios of 10 [NASA TN D-921] (Record no. 563731)

000 -LEADER
fixed length control field 00777nam a2200193 4500
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20201230163259.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 201230b xxu||||| |||| 00| 0 eng d
040 ## - CATALOGING SOURCE
Transcribing agency IIT Kanpur
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title eng
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name Dixon, Sidney C.
245 ## - TITLE STATEMENT
Title Experimental investigation at mach number 3.0 of the effects of thermal stress and buckling on the flutter of four bay aluminium alloy panels with length width ratios of 10 [NASA TN D-921]
Statement of responsibility, etc Sidney C. Dixon, George E. Griffith and Herman L. Bohon
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication Washington, D. C.
Name of publisher National Aeronautics and Space Administration
Year of publication 1961
300 ## - PHYSICAL DESCRIPTION
Number of Pages 28p
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title National Aeronautics and Space Administration (NASA)
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Thermal stress
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Griffith, George E.
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Bohon, Herman L.
942 ## - ADDED ENTRY ELEMENTS (KOHA)
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