Optimising stator vane settings in multistage axial flow compressors
, 2002 There is a common requirement in the process, oil and gas turbine industries for high performance axial flow compressors operating over a wide range of mass flow rate and rotational speed at high efficiency. The trends have been for higher blade loadings (greater pressure rise per stage) and higher efficiency which are increasingly achieved through ...
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End-to-end design of multistage high-pressure axial compressor for a promising aviation gas turbine engine [PDF]
Evgeny S. Goryachkin, I. Kudryashov
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Experimental Study to Quantify Fracture Propagation in Hydraulic Fracturing Treatment. [PDF]
ACS Omega, 2022 He P, Pan L, Lu Z, Zhou J, Meng C, Yu H.
europepmc +1 more source
Model equation for simulating flows in multistage turbomachinery [PDF]
A steady, three-dimensional average-passage equation system is derived for use in simulating multistage turbomachinery flows. These equations describe a steady, viscous flow that is periodic from blade passage to blade passage.
Adamczyk, J. J.
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A Resistivity Plate Loading Device for Assessing the Factors Affecting the Stiffness of a Cement-Stabilized Subgrade. [PDF]
Materials (Basel), 2022 Feng H, Siaw AF, Wang H.
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Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer [PDF]
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital computer is presented. The method involves linearization of nonlinear dynamic equations about an operating point on a speed line, and then application of ...
Blaha, R. J. +2 more
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Analysis and modeling of non-synchronous aeroelastic phenomena in an axial multistage compressor
, 2021 Anne-Lise Fiquet
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Effect of slotted casing treatment on performance of a multistage compressor [PDF]
A J85-13 engine was equipped with a compressor case that allowed changes to the case wall over the rotor tips of six of its eight stages. The engine was tested with four inlet configurations: uniform inlet flow, 180 degree circumferential distortion, hub
Moss, J. E., Jr.
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Design of a miniature hydrogen fueled gas turbine engine [PDF]
The design, development, and delivery of a miniature hydrogen-fueled gas turbine engine are discussed. The engine was to be sized to approximate a scaled-down lift engine such as the teledyne CAE model 376.
Burnett, M. +6 more
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Single-stage experimental evaluation of boundary layer blowing techniques for high lift stator blades. 1 - Compressor design [PDF]
Boundary layer blowing techniques for high lift stator blades in axial flow ...
Chapman, D. C., Miller, M. L.
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