To Study the effect of Reynolds number and Thickness Ratio on Aerodynamic Performance of an Airfoil (Record no. 323384)

000 -LEADER
fixed length control field 00421 a2200145 4500
001 - CONTROL NUMBER
control field 88311
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number PR 508
090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN)
-- 41731
-- 41731
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Fahad Memon
245 ## - TITLE STATEMENT
Title To Study the effect of Reynolds number and Thickness Ratio on Aerodynamic Performance of an Airfoil
Statement of responsibility, etc. Hossein Raza Hamdhani
Name of part/section of a work CAEG-53 (A)
250 ## - EDITION STATEMENT
Edition statement 1st
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Risalpur
Name of publisher, distributor, etc. NUST
Date of publication, distribution, etc. 2001
300 ## - PHYSICAL DESCRIPTION
Extent 52p
500 ## - GENERAL NOTE
General note BE Project Reports
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Institution code [OBSOLETE] CAE NUST
Call number prefix PR 508
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Total Checkouts Full call number Barcode Date last seen Price effective from Koha item type
          College of Aeronautical Engineering (CAE) College of Aeronautical Engineering (CAE) 04/03/2017   PR 508 CAEPR-508 04/05/2017 04/05/2017 Book
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