To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil (Record no. 323360)

000 -LEADER
fixed length control field 00477 a2200145 4500
001 - CONTROL NUMBER
control field 88287
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number PR-516
090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN)
-- 41706
-- 41706
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Saifur Rehman Bakaul
245 ## - TITLE STATEMENT
Title To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil
Statement of responsibility, etc. Hussein Raza Hamdani
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 98p
500 ## - GENERAL NOTE
General note BE- Project Report
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Institution code [OBSOLETE] CAE NUST
Call number prefix PR-516
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Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Total Checkouts Full call number Barcode Date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-516 CAEPR-516 04/05/2017 04/05/2017 Book
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