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THEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW (Record no. 397146)

000 -LEADER
fixed length control field	00433pam a2200133a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	TN D-4929
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Queijo,M J
245 1# - TITLE STATEMENT
Title	THEORY FOR COMPUTING SPAN LOADS AND STABILITY DERIVATIVES DUE TO SIDESLIP YAWING AND ROLLING FOR WINGS IN SUBSONIC COMPRESSIBLE FLOW
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc.	Nasa, Washington, D.C.
Date of publication, distribution, etc.	1968
300 ## - PHYSICAL DESCRIPTION
Extent	76
500 ## - GENERAL NOTE
General note	Bound With Nasa Tn D-4921-28, 4930.
964 ## -
--	CIRC
997 ## -
--	TR12449 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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-4929	TR12449	2016-05-19	2016-05-19	Technical Report

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