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To design a rocket nozzle study its heat transfer characteristics and then design a suitable cooling system for the nozzle

By: Muhammad NaeemPublisher: Karachi NED 1983Description: 105p. Khalid PervezDDC classification: PR 842

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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 842 (Browse shelf)	Available		CAEPR-842

Total holds: 0

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Previous	PR 84 Design and development of an FPGA based cryptographic system	PR 840 Aerodynamic design of man powered aircraft	PR 841 Boundary Layer control	PR 842 To design a rocket nozzle study its heat transfer characteristics and then design a suitable cooling system for the nozzle	PR 843 Vibration analysis of an aircraft wing (using analog computer)	PR 844 Design and fabrication of subsonic open circuit wind tunnel	PR 845 Study of the laminar boundary layer theory	Next

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