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To Formulate a Computer Code for Designing a Blade of an Axial Flow Compressor, Using Free Votex Concept 49 "A" EC

By: Farukh HussainPublisher: Karachi NED University 1998Description: 62pDDC classification: PR 1287

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Item type	Current location	Home library	Collection	Call number	Status	Date due	Barcode	Item holds
Book	College of Aeronautical Engineering (CAE)	College of Aeronautical Engineering (CAE)	NFIC	PR 1287 (Browse shelf)	Available		CAEPR-1287

Total holds: 0

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Previous	PR 1283 Airfoil Shape Optimization by Analytical Methods inthe transonic Region	PR 1284 To Determine the Airfoil used on the Wings of Mushshak A/C and its comparison with NASA Airfoil Family	PR 1285 Simulation of Airflow Pattern Inside Air Intake	PR 1287 To Formulate a Computer Code for Designing a Blade of an Axial Flow Compressor, Using Free Votex Concept	PR 1288 Formulation of Code for 2-D Heat Transfer	PR 1289 Modelling of a Logistic Forecasting System	PR 129 Identification and analysis of high stress areas of C-130 outer wing using statistical techniques and finite element method	Next

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