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AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4(DEGRE) TO 100(DEGRE) OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS (Record no. 397315)

000 -LEADER
fixed length control field	00522pam a2200133a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	TM X-288
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Spencer,Bernard
245 1# - TITLE STATEMENT
Title	AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4(DEGRE) TO 100(DEGRE) OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa,Washington, D.C.
Date of publication, distribution, etc.	1960
300 ## - PHYSICAL DESCRIPTION
Extent	28
500 ## - GENERAL NOTE
General note	Bound With Nasa Tm X-281-283,289-299,Lack No. 282,84-87,90,93,95,96,98
964 ## -
--	CIRC
997 ## -
--	TR13674 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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-288	TR13674	2016-05-19	2016-05-19	Technical Report

PKK Library