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To develop a computer program for determination of thermal fatigue life consumption of a HPT blade (from available temperature history)

By: Hamid Bin Hameed, 016117Publisher: Risalpur NUST Risalpur 2005Description: ix, 90p. Muhammad Naeem , DrDDC classification: PR 355

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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 355 (Browse shelf)	Available		CAEPR-355

Total holds: 0

Previous	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	No cover image available	Next
Previous	PR 352 Performance analysis of an ejector nozzle	PR 353 Numerical study of flow behaviour over a delta wing W.R.T change in aspect ratio and sweep back angle	PR 354 Using panel methods to study the effect of wing planform on aerodynamic characteristics of wing and compare the results with commercial software	PR 355 To develop a computer program for determination of thermal fatigue life consumption of a HPT blade (from available temperature history)	PR 356 To develop a computer program for determination of creep life consumption of a HPT blade (from available temperature history)	PR 357 Force and flow at low reynolds number during hovering motion	PR 358 To determine the aerodynamic co-efficients of JF-17 standard-1 weapons	Next

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