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WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE (Record no. 394791)

000 -LEADER
fixed length control field	00489pam a2200133a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	TM X-179 -
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Fournier,Paul G
245 1# - TITLE STATEMENT
Title	WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE
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	21
500 ## - GENERAL NOTE
General note	Bound With Nasa Tm X-165-79
964 ## -
--	CIRC
997 ## -
--	TR8836 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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 TM X-179 -	TR8836	2016-05-19	2016-05-19	Technical Report

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