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EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM.. (Record no. 394384)

000 -LEADER
fixed length control field	00540pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	TN D-1959 -
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Goldberg,Theodore J
245 1# - TITLE STATEMENT
Title	EFFECTS OF ROUNDING CORNERS AND LEADING EDGES ON THE WINDWARD-SURFACE PRESSURE OF A DELTA WING SWEPT 65(DG) AT A MACH NUMBER OF 5.96 AT ANGLES OF ATTACK FROM 65(DG) TO 115(DG)AND ANGLES OF ROLL FROM..
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa, Washington, D.C.
Date of publication, distribution, etc.	1963
300 ## - PHYSICAL DESCRIPTION
Extent	34
500 ## - GENERAL NOTE
General note	Bound With Nasa Tn D-1951-1960
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Blanchard,Doris K
964 ## -
--	CIRC
997 ## -
--	TR8715 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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 TN D-1959 -	TR8715	2016-05-19	2016-05-19	Technical Report

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