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BOUNDARY LAYER DEVELOPMENT IN AXIAL COMPRESSORS AND TURBINES. PART 4 OF 4: COMPUTATIONS & ANALYSES

Citation

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 4 OF 4: COMPUTATIONS & ANALYSES, International Gas Turbine and Aeroengine Congress and Exposition, Houston, Texas, U.S.A., pp. 1-16. (1995) [Refereed Conference Paper]

Item Details

Item Type:Refereed Conference Paper
Research Division:Engineering
Research Group:Aerospace Engineering
Research Field:Aerospace Engineering not elsewhere classified
Objective Division:Expanding Knowledge
Objective Group:Expanding Knowledge
Objective Field:Expanding Knowledge in Philosophy and Religious Studies
Author:Walker, GJ (Professor Greg Walker)
ID Code:4544
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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