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Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836] (Record no. 399904)

000 -LEADER
fixed length control field 00671pam a2200181a 44500
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200624114709.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 200624b 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 Kehlet, Alan B.
245 1# - TITLE STATEMENT
Title Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket -propelled airplane configuration having a low 52.5 (degree) delta wing and an unswept horizontal tail [NASA TN D-836]
Statement of responsibility, etc Alen B. Kehlet
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher Nasa
Year of publication 1961
Place of publication Washington, D.C.
300 ## - PHYSICAL DESCRIPTION
Number of Pages 26p
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title National Aeronautics and Space Administration (NASA)
505 ## - FORMATTED CONTENTS NOTE
Formatted contents note NASA technical report
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Aerodynamic
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Full call number Accession Number Koha item type
        COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2007-08-12 NASA TN D-836 TR16137 Technical Report

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