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Investigation of boundary layer on a flat plate with zero pressure gradient in CAE subsonic wind tunnel

By: Tariq MuzaffarPublisher: Karachi University of Karachi 1977Description: 40p. BakhtiarDDC classification: PR 726

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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 726 (Browse shelf)	Available		CAEPR-726

Total holds: 0

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Previous	PR 723 Symmetrical and unsymmetrical bending of cantilever beams	PR 724 Fuselage pannels with various stiffness are to be fabricated, buckling tests to be performed on universal testing machine, results to be compared with theory	PR 725 Development of the technique for use of fatigue gauges	PR 726 Investigation of boundary layer on a flat plate with zero pressure gradient in CAE subsonic wind tunnel	PR 727 Drag versus mach number studies on computer	PR 728 Calibration of supersonic wind tunnel sting balance	PR 729 Flight testing for specific Excesspower on F-6	Next

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