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RISDiscussion: “Boundary-Layer Development on an Axial-Flow Compressor Stator Blade” (Evans, R. L., 1978, ASME J. Eng. Power, 100, pp. 287–292)
Publisher: The American Society of Mechanical Engineers (ASME)
A Family of Surface Velocity Distributions for Axial Compressor Blading and Their Theoretical Performance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The influence of free stream disturbances on transition is discussed and it is noted that significant regions of laminar flow may exist on axial turbomachine blades despite the high level of ...
Closure to “Discussion of ‘The Role of Laminar-Turbulent Transition in Gas Turbine Engines: A Discussion’” (1993, ASME J. Turbomach., 115, pp. 216–217)
Publisher: The American Society of Mechanical Engineers (ASME)
The Role of Laminar-Turbulent Transition in Gas Turbine Engines: A Discussion
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An extended discussion of Mayle’s (1991) critical study of transition phenomena in gas turbine engines is presented. Attention is focused on transition in decelerating flow regions, which are ...
Discussion: “Measurements of Wake-Generated Unsteadiness in the Rotor Passages of Axial Flow Turbines” (Hodson, H. P., 1985, ASME J. Eng. Gas Turbines Power, 107, pp. 467–475)
Publisher: The American Society of Mechanical Engineers (ASME)
Discussion: “Periodically Unsteady Flow in an Imbedded Stage of a Multistage, Axial-Flow Turbomachine” (Wagner, J. H., Okiishi, T. H., and Holbrook, G. J., 1979, ASME J. Eng. Power, 101, pp. 42–51)
Publisher: The American Society of Mechanical Engineers (ASME)
Closure to “Discussion of ‘Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels’” (1991, ASME J. Turbomach., 113, p. 624)
Publisher: The American Society of Mechanical Engineers (ASME)
Similarity Behavior in Transitional Boundary Layers Over a Range of Adverse Pressure Gradients and Turbulence Levels
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Boundary layer transition has been investigated experimentally under low, moderate, and high free-stream turbulence levels and varying adverse pressure gradients. Under high turbulence levels and ...
Effects of Adverse Pressure Gradients on the Nature and Length of Boundary Layer Transition
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Existing transition models are surveyed and deficiencies in previous predictions, which seriously overestimate transition length under an adverse pressure gradient, are discussed. A new model for ...
Natural Transition Phenomena on an Axial Compressor Blade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Data from a surface hot-film array on the outlet stator of a 1.5-stage axial compressor are analyzed to look for direct evidence of natural transition phenomena. An algorithm is developed to ...