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Modification of an existing code of turbo ramjet engine in FORTRAN 77 to include the effects of changing bypass ratio for the engine operation G-58

By: Shakeel Virk Muhammad; Naeem Khan, ProfPublisher: Risalpur NUST 2003Description: xi, 125 pDDC classification: PR 315

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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 315 (Browse shelf)	Available		CAEPR-315

Total holds: 0

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Previous	PR 312 Modeling of frame 6 of super mushshak aircraft using solid edge software and its analysis in ANSYS software	PR 313 Modeling of frame 5 of super mushshak aircraft in solid edge and its analysis in ANSYS	PR 314 To study the delay in boundry layer seperation under the combined affect of oscillation and heat induction to NACA 0012 airfoil	PR 315 Modification of an existing code of turbo ramjet engine in FORTRAN 77 to include the effects of changing bypass ratio for the engine operation	PR 316 Theoretical Investigation of pressure differential angle attack measurement system	PR 318 To Study the possibility of provisioning of Air Conditioning of Y-12 aircraft which could provide adequate cooling on ground and during low level flight	PR 319 High angle of attack and high mack number performance estimation of JF-17 thunder using corrected wind tunnel test data	Next

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