NUST Institutions Library Catalogue catalog › Details for: To develop pressure data acquisition system for CAE closed circuit subsonic wind tunnel, using pressure distribution from CFD and to calibrate and configure the system using analog voltage signal

Normal view MARC view ISBD view

To develop pressure data acquisition system for CAE closed circuit subsonic wind tunnel, using pressure distribution from CFD and to calibrate and configure the system using analog voltage signal G-62

By: Intizar Ahmed; Atiq ur rehman; Jehanzeb masood; ishaat saboor advisorsPublisher: Risalpur NUST 2007Description: ix, 77 pDDC classification: PR 378

Tags from this library: No tags from this library for this title. Log in to add tags.

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 378 (Browse shelf)	Available		CAEPR-378

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 375 Using lab view software design and fabriate PC based prototype systems for test and measurement	PR 376 Design and fabrication of an aerial pesticide atomizer	PR 377 Non linear contact analysis of Lug joints of wing fuselage attachment of JF-17 aircraft	PR 378 To develop pressure data acquisition system for CAE closed circuit subsonic wind tunnel, using pressure distribution from CFD and to calibrate and configure the system using analog voltage signal	PR 379 Study / analysis of brake system failure on super mushshak aircraft and to propose modified system	PR 38 Design and development of Anomaly Detection Scheme for manets in NS2	PR 380 to implement a generic fighter aircraft one dimensional longitudinal flight controls (pitch mode) using simulation techniques and implement it physically so as to simulate various flight stability charactertics and dynamic properties of the aircraft	Next

BE project reports

There are no comments on this title.

to post a comment.