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BOUNDARY LAYER DEVELOPMENT IN AXIAL COMPRESSORS AND TURBINES. PART 2 OF 4: COMPRESSORS
conference contribution
posted on 2023-05-23, 02:18 authored by Halstead, DE, Wisler, DC, Okiishi, TH, Walker, GJ, Hodson, HP, Shin, HWNo description available
History
Volume
ASME Paper 95-GT-462Pagination
1-20Department/School
School of EngineeringPublisher
The American Society of Mechanical EngineersEvent title
International Gas Turbine and Aeroengine Congress and ExpositionEvent Venue
Houston, Texas, U.S.A.Date of Event (Start Date)
1995-01-01Date of Event (End Date)
1995-01-01Repository Status
- Restricted
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