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Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974] (Record no. 399182)

000 -LEADER
fixed length control field 00673pam a2200193a 44500
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200623122906.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 200623b 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 Bennett, Floyd V.
245 1# - TITLE STATEMENT
Title Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974]
Statement of responsibility, etc Floyd V. Bennett
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher Nasa, Washington, D.C.
Year of publication 1961
300 ## - PHYSICAL DESCRIPTION
Number of Pages 41p
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title National Aeronautics and Spce Administratio (NASA)
500 ## - GENERAL NOTE
General note Bound With Nasa Tn D-971-973,975-980
505 ## - FORMATTED CONTENTS NOTE
Formatted contents note Technical Note D-974
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Aeroelastic
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Reference
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Accession Number Koha item type
        COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2007-08-12 TR13289 [TN D-974] Technical Report

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