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THE EFFECT OF CONICAL THICKNESS DISTRIBUTIONS ON THE SEPRATED FLOW PAST SLENDER DELTA WINGS. (Record no. 397828)

000 -LEADER
fixed length control field 00405pam a2200133a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number ARC
Item number C.P 1189
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Portnoy,H
245 1# - TITLE STATEMENT
Title THE EFFECT OF CONICAL THICKNESS DISTRIBUTIONS ON THE SEPRATED FLOW PAST SLENDER DELTA WINGS.
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc. Her Majesty'S Stationery Office, London
Date of publication, distribution, etc. 1971
300 ## - PHYSICAL DESCRIPTION
Extent 15
500 ## - GENERAL NOTE
General note Bound With Arc Cp-1181-1188,1190.
964 ## -
-- CIRC
997 ## -
-- TR14462 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Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Full call number Barcode Date last seen Price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 ARC C.P 1189 TR14462 2016-05-19 2016-05-19 Technical Report

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