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FORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS (Record no. 393201)

000 -LEADER
fixed length control field	00448pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	MEMO 4-3-59L -
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Margolis,Kenneth
245 1# - TITLE STATEMENT
Title	FORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa, Washington, D.C.
Date of publication, distribution, etc.	1959
300 ## - PHYSICAL DESCRIPTION
Extent	26
500 ## - GENERAL NOTE
General note	Bound With Nasa Memo 4-1-59l-4-19-59l
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Elliott,Miriam H
964 ## -
--	CIRC
997 ## -
--	TR7688 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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
		Untraceable		General Stacks	PK Kelkar Library, IIT Kanpur	PK Kelkar Library, IIT Kanpur	2007-08-12	NASA MEMO 4-3-59L -	TR7688	2016-05-19	2016-05-19	Technical Report

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