Normal view MARC view ISBD view

EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01 (Record no. 393202)

000 -LEADER
fixed length control field	00506pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	NASA
Item number	MEMO 4-4-59L -
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name	Spearman,M Leroy
245 1# - TITLE STATEMENT
Title	EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01
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	28
500 ## - GENERAL NOTE
General note	Bound With Nasa Memo 4-1-59l-4-19-59l
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Driver,Cornelius
964 ## -
--	CIRC
997 ## -
--	TR7689 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Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Full call number	Barcode	Date last seen	Price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 MEMO 4-4-59L -	TR7689	2016-05-19	2016-05-19	Technical Report

PKK Library