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Development of Airfoil which gives the desired Pressure Distribution, using IBM PC 42 "A" EC

By: Yousaf Haroon Ansari; Muhammad Ismail and Salman Absar (Advisors)Publisher: Karachi NED university 1995Description: 70pDDC classification: PR 1189

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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 1189 (Browse shelf)	Available		CAEPR-1189

Total holds: 0

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Previous	PR 1186 Study of Pitot-Static Indication System to Determine the Causes and Extent of Error and to make a Potential Flow Model Using Panel Method	PR 1187 Instrumentation of 1"x1" Wind Tunnel using Scanivalve system and Computerized DAQ System is to be installed	PR 1188 Aerodynamics of Strake-Wind Combination	PR 1189 Development of Airfoil which gives the desired Pressure Distribution, using IBM PC	PR 119 Study and implementation of MIL-STD-1553 avionics data bus on FPGA	PR 1190 Determination of Stress Intensity Factor by using COSMOS/M and Comparison with Existing Data	PR 1191 Study of Base Cavity on Base Pressure in Supersonic flow over an Axisymmetric Body	Next

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