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LOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES (Record no. 401952)

000 -LEADER
fixed length control field	00554pam a2200133a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	MEMO 1-22-59L
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Boisseau,Peter C
245 1# - TITLE STATEMENT
Title	LOW-SUBSONIC STATIC STABILITY AND DAMPING DERIVATIVES AT ANGLES OF ATTACK FROM 0 DEGREE TO 90 DEGREE FOR A MODEL WITH A LOW-ASPECT-RATIO UNSWEPT WING AND TWO DIFFERENT FUSELAGE FOREBODIES
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	25
500 ## - GENERAL NOTE
General note	Bound With Nasa Memo 1-15-59l-20,23-31 Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
964 ## -
--	CIRC
997 ## -
--	TR17736 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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 1-22-59L	TR17736	2016-05-19	2016-05-19	Technical Report

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