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FLOW FIELD ANALYSIS OF AIRCRAFT CONFIGURATION USING A NUMERICAL SOLUTION TO THE THREE-DIMENSIONAL UNIFIED SUPERSONIC/HYPERSONIC SMALL-DISTURBENCE EQUATIONS (Record no. 393017)

000 -LEADER
fixed length control field	00500pam a2200145a 44500
040 ## - CATALOGING SOURCE
Original cataloging agency	P K Kelkar Library, IIT Kanpur
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	CR-1926
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Gunness,C.
245 1# - TITLE STATEMENT
Title	FLOW FIELD ANALYSIS OF AIRCRAFT CONFIGURATION USING A NUMERICAL SOLUTION TO THE THREE-DIMENSIONAL UNIFIED SUPERSONIC/HYPERSONIC SMALL-DISTURBENCE EQUATIONS
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa, Washington, D.C.
Date of publication, distribution, etc.	1972
300 ## - PHYSICAL DESCRIPTION
Extent	114
500 ## - GENERAL NOTE
General note	Bound With Nasa Cr-1921-28
964 ## -
--	CIRC
997 ## -
--	TR8346 C

Holdings
Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price effective from	Koha item type
				General Stacks	PK Kelkar Library, IIT Kanpur	PK Kelkar Library, IIT Kanpur	2007-08-12	NASA CR-1926	TR8346	2016-05-19	2016-05-19	Technical Report

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