Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade, by Roy G. Stabe et al.

Title:	Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade
Author:	Stabe, Roy G.
Author:	Kline, John F.
Author:	Lewis Research Center
Note:	National Aeronautics and Space Administration ;, 1975

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Subject:	Air flow
Subject:	Aircraft gas-turbines -- Blades -- Cooling
Subject:	Cascade flow
Subject:	Cascades (Fluid dynamics)
Subject:	Cooling systems
Subject:	Flow characteristics
Subject:	Heat -- Transmission
Subject:	Pressure measurement
Subject:	Thermodynamic properties
Subject:	Turbine blades
Subject:	Turbine engines
Subject:	Turbines -- Aerodynamics
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