Search
Now showing items 1-6 of 6
Loss Reduction Using Riblets on a Supersonic Through-Flow Fan Blade Cascade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental and computational study to determine the effects of riblets on the performance of the Supersonic Throughflow Fan (STF) cascade blades was performed. The cascade was tested in ...
Performance and Flow Characteristics of an Optimized Supercritical Compressor Stator Cascade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental and numerical study was performed on an optimized compressor stator cascade designed to operate efficiently at high inlet Mach numbers (M1) ranging from 0.83 to 0.93 (higher ...
Supersonic Through-Flow Fan Blade Cascade Studies
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An investigation has been performed of the flow in a supersonic through-flow fan blade cascade. The blade shapes are those of the baseline supersonic through-flow fan (STF). Measurements were ...
Experimental Reduction of Transonic Fan Forced Response by Inlet Guide Vane Flow Control
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The main contributor to the high cycle fatigue of compressor blades is the response to aerodynamic forcing functions generated by an upstream row of stators or inlet guide vanes. Resonant ...
Aerodynamic Design and Testing of Three Low Solidity Steam Turbine Nozzle Cascades
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Three sets of low solidity steam turbine nozzle cascades were designed and tested. The objective was to reduce cost through a reduction in parts count while maintaining or improving performance. ...
Experimental Investigation of the Effects of a Moving Shock Wave on Compressor Stator Flow
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Linear cascade testing was performed to simulate the flow conditions experienced by stator blades in an axial compressor with supersonic relative Mach numbers at the inlet to the downstream ...
CSV
RIS