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THE STATIC AND DYNAMIC ROTARY STABILITY DERIVATIVES AT SUBSONIC SPEEDS ON AN AIRPLANE MODEL HAVING WING AND TAIL SURFACES SWEPT BACK 45 (Record no. 396751)

000 -LEADER
fixed length control field	00525pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	MEMO 5-16-59A
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Lopez,Armando E,Buell,Donald A
245 1# - TITLE STATEMENT
Title	THE STATIC AND DYNAMIC ROTARY STABILITY DERIVATIVES AT SUBSONIC SPEEDS ON AN AIRPLANE MODEL HAVING WING AND TAIL SURFACES SWEPT BACK 45
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	75
500 ## - GENERAL NOTE
General note	Bound With Nasa Memo 5-12-59a,5-18-59a-5-20-59a Lack No. 13-15,17,19
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Tinling,Bruce E
964 ## -
--	CIRC
997 ## -
--	TR11440 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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 MEMO 5-16-59A	TR11440	2016-05-19	2016-05-19	Technical Report

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