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of 3
pro vyhledávání: '"Gregory Laskowski"'
Publikováno v:
Volume 5B: Heat Transfer.
Fast response pressure data acquired in a high-speed 1.5-stage turbine Hot Gas Ingestion Rig shows the existence of pressure oscillation modes in the rim-seal-wheelspace cavity of a high pressure gas turbine stage with purge flow. The experimental re
Publikováno v:
Volume 5B: Heat Transfer.
Pressure sensitive paint (PSP) can be a powerful tool in measuring the adiabatic film cooling effectiveness. There are two distinct sources of error for this measurement technique; the ability to experimentally obtain the data and the validity of the
Publikováno v:
Volume 5: Heat Transfer, Parts A and B.
Aircraft turbine blade trailing edges commonly are cooled by blowing air through pressure-side cutback slots. The surface effectiveness is governed by the rate of mixing of the coolant with the mainstream, which is typically much faster than predicte