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

conference contribution
posted on 2023-05-23, 02:18 authored by Halstead, DE, Wisler, DC, Okiishi, TH, Walker, GJ, Hodson, HP, Shin, HW
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History

Volume

ASME Paper 95-GT-464

Pagination

1-16

Department/School

School of Engineering

Publisher

The American Society of Mechanical Engineers

Event title

International Gas Turbine and Aeroengine Congress and Exposition

Event Venue

Houston, Texas, U.S.A.

Date of Event (Start Date)

1995-01-01

Date of Event (End Date)

1995-01-01

Repository Status

  • Restricted

Socio-economic Objectives

Expanding knowledge in philosophy and religious studies

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