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Feasibility study of Testing Pneumatic Selas at High Temperature and pressure for Aircraft Component Adbiser 37:A: EC

By: Shabbir; Prof Naeem and Prof Niazi (Advisors)Publisher: Karachi NED University 1992Description: 131pDDC classification: PR 1101

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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 1101 (Browse shelf)	Available		CAEPR-1101

Total holds: 0

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Previous	PR 11 Study and implementation of MIL-STD-1553 Avionics data bus on FPGA for interface with R&S radios (Phase-II)	PR 110 Development of a test rig for aircraft electrical harnesses	PR 1100 To Study the Possibility of Incressing the Capicity of Fuel in Mushshak Aircraft	PR 1101 Feasibility study of Testing Pneumatic Selas at High Temperature and pressure for Aircraft Component Adbiser	PR 1102 Construction and Optimization of Fly away Kit for a Particular Flying Squadron	PR 1103 Continuation of Pilots Gondola Integration with Rotating Arm and Control Cabin	PR 1104 To study the Tooling Requirement for Manufacturing Jet Aircraft	Next

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