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Effects of Transient Heat Transfer on Compressor Stability
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The effects of heat transfer between the compressor structure and the primary gas path flow on compressor stability are investigated during hot engine re-acceleration transients. A mean line analysis of an advanced, ...
Forced Response System Identification of Full Aero-Engine Rotordynamic Systems for Prognostics and Diagnostics
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A first-of-its-kind forced-response system identification approach is introduced to measure rotordynamic damping of shaft modes in a full gas turbine aero-engine. The approach involves forced-response modal analysis in ...
An Investigation of Condensation Effects in Supercritical Carbon Dioxide Compressors
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Supercritical CO2 (SCO2) power cycles have demonstrated significant performance improvements in concentrated solar and nuclear applications. These cycles promise an increase in thermaltoelectric conversion efficiency of ...
Low Flow Coefficient Centrifugal Compressor Design for Supercritical CO2
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a design strategy for very low flow coefficient multistage compressors operating with supercritical CO2 for carbon capture and sequestration (CCS) and enhanced oil recovery (EOR). At flow coefficients ...
Drag Management in High Bypass Turbofan Nozzles for Quiet Approach Applications
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The feasibility of a drag management device that reduces engine thrust on approach by generating a swirling outflow from the fan (bypass) nozzle is assessed. Deployment of such “engine airbrakes†(EABs) can assist in ...
Dynamic Model-Based Identification of Cavitation Compliance and Mass Flow Gain Factor in Rocket Engine Turbopump Inducers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Cavitation dynamics continue to pose a significant risk in the development and operation of launch vehicle (LV) propulsion systems. In addition to generating unsteady loads that can directly damage turbopump hardware, ...
Origins and Structure of Spike Type Rotating Stall
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: In this paper, we describe the structures that produce a spiketype route to rotating stall and explain the physical mechanism for their formation. The descriptions and explanations are based on numerical simulations, ...
The Role of Tip Leakage Flow in Spike-Type Rotating Stall Inception
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper describes the role of tip leakage flow in creating the leading edge separation necessary for the onset of spike-type compressor rotating stall. A series of unsteady multipassage simulations, supported by ...