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BOUNDARY LAYER DEVELOPMENT IN AXIAL COMPRESSORS AND TURBINES. PART 3 OF 4: LP TURBINES

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Halstead, DE and Wisler, DC and Okiishi, TH and Walker, GJ and Hodson, HP and Shin, HW, BOUNDARY LAYER DEVELOPMENT IN AXIAL COMPRESSORS AND TURBINES. PART 3 OF 4: LP TURBINES, International Gas Turbine and Aeroengine Congress and Exposition, Houston, Texas, U.S.A., pp. 1-15. (1995) [Refereed Conference]

Item Type:	Refereed Conference
Subjects:	Engineering
Subjects:	Aerospace Engineering
Subjects:	Aerospace Engineering not elsewhere classified
Subjects:	Expanding Knowledge
Subjects:	Expanding Knowledge
Subjects:	Expanding Knowledge in Philosophy and Religious Studies
Creator:	Walker, GJ (Professor Greg Walker)
ID Code:	4543
Year Published:	1995
Deposited By:	Civil and Mechanical Engineering
Deposited On:	1995-08-01
Last Modified:	1996-02-01
Downloads:	0

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