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Conceptual Desig of a Dual-mode Scramjet Propulsion System for Integration to a Hypersonic Cruise Vehicle in Booster Configuration 77 "A" EC

By: Qasim Manzoor; Prof Ali Sarosh and Shuaib Salamat (Advisors)Publisher: Islamabd NUST 2014Description: 99pDDC classification: PR 2474

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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 2474 (Browse shelf)	Available		CAEPR-2474

Total holds: 0

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Previous	PR 2471 Multi Disciplinary Design Optimization of an Aircraft	PR 2472 Modeling of Fixed wing UAV for Fightgear and Designing its Autopilot in MATLAB Simulink	PR 2473 Constrained Torsional Analysis of Multicell Composite Thin Walled Tapered Beams	PR 2474 Conceptual Desig of a Dual-mode Scramjet Propulsion System for Integration to a Hypersonic Cruise Vehicle in Booster Configuration	PR 2475 Numerical Simulation Based Assessment for Stage-separation Aerothermodynamics of a Pick-a-back Two-stage-to-orbit (TSTO) Space plane configuration	PR 2476 feasibility Study to Adapt existing engine Test Bed of T-37 A/C for engine of K-8 A/C (Phase II Manufaturing and Financial Estimates)	PR 2477 Material Characterization of Composite Materials under varying strain rates	Next

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