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EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS (Record no. 398695)

000 -LEADER
fixed length control field	00592pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	TM X-519
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Robinson,Ross B
245 1# - TITLE STATEMENT
Title	EFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa, Washington, D.C.
Date of publication, distribution, etc.	1961
300 ## - PHYSICAL DESCRIPTION
Extent	17
500 ## - GENERAL NOTE
General note	Bound With Nasa Tm X-507-18,522-81, Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Spearman,M Leroy
964 ## -
--	CIRC
997 ## -
--	TR14307 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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 TM X-519	TR14307	2016-05-19	2016-05-19	Technical Report

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