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A FLIGHT AND WIND TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE-OF-ATTACK RATE ON MAXIMUM LIFT COEFFICIENT (Record no. 448337)

000 -LEADER
fixed length control field	00423pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	CR-321
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Conner,F,Willey,C
245 1# - TITLE STATEMENT
Title	A FLIGHT AND WIND TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE-OF-ATTACK RATE ON MAXIMUM LIFT COEFFICIENT
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa, Washington, D.C.
Date of publication, distribution, etc.	1965
300 ## - PHYSICAL DESCRIPTION
Extent	51
500 ## - GENERAL NOTE
General note	Bound With Nasa Cr-322-24.
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Twomey,W
964 ## -
--	CIRC
997 ## -
--	64883 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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-321	64883	2016-05-19	2016-05-19	Technical Report

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