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WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A MODEL REPRESENTATIVES OF A SUPERSONIC FIGHTER-CLASS AIRPLANE WITH AN EXTERNAL-FLOW JET-AUGMENTED FLAP IN LOW-SPEED FLIGHT [NASA TN D-50] (Record no. 395297)

000 -LEADER
fixed length control field 00653pam a2200169a 44500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20221125104633.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 221125b 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 Newson, William A.
245 1# - TITLE STATEMENT
Title WIND-TUNNEL INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A MODEL REPRESENTATIVES OF A SUPERSONIC FIGHTER-CLASS AIRPLANE WITH AN EXTERNAL-FLOW JET-AUGMENTED FLAP IN LOW-SPEED FLIGHT [NASA TN D-50]
Statement of responsibility, etc Newson William A.
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher National Aeronautics and Space Administration
Year of publication 1959
Place of publication Washington, D.C.
300 ## - PHYSICAL DESCRIPTION
Number of Pages 84p
500 ## - GENERAL NOTE
General note Bounds vol. contains NASA TN D 41-50
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Technical Report
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Serial Enumeration / chronology Accession Number Koha item type
        COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2007-08-12 NASA TN D 41-50 TR010898 Technical Report

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