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RISAerodynamic Design and Verification of a Two-Stage Turbine With a Supersonic First Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The detailed aerodynamic design and test verification of a 6000-hp (4474-kW) turbine with a supersonic first stage for an airborne application is described. The 12.3-in. (312.4-mm) pitch diameter ...
Investigation of Rotor Blade Roughness Effects on Turbine Performance
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The cold air test program was completed on the SSME (Space Shuttle Main Engine) HPFTP (High-Pressure Fuel Turbopump) turbine with production nozzle vane rings and polished coated rotor blades ...