Results 91 to 100 of about 631 (221)
Journal of the Global Power and Propulsion Society, 2018 The basic tool set to design multi-stage axial compressors consists of fast codes for throughflow and blade-to-blade analysis. Detailed blade row design is conducted with 3D CFD, mainly to control the end wall flow.
Markus Schnoes +2 more
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MULTISTAGE AXIAL COMPRESSOR MAP GENERATION
, 1993 A one-dimensional theory regarding the change of state in a multistage axial compressor at design point and part load has been formulated. With regard to short calculation times for obtaining compressor maps this algorithm is suitable to get insight into
KÓBOR, Ágota
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Modelling & integration of advanced propulsion systems [PDF]
, 2008 This research study focuses on the design of advanced propulsion cycles, having as primary design goal the improvement on noise emissions and fuel consumption.
Doulgeris, Georgios C.
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Considerations for High-Fidelity Modeling of Unsteady Flows in a Multistage Axial Compressor
International Journal of Turbomachinery, Propulsion and PowerThis paper presents the development and validation of a high-fidelity, unsteady, computational fluid dynamics (CFD) model of the Purdue 3-Stage Axial Research Compressor. A grid convergence study assesses the spatial discretization accuracy of the single-
Douglas R. Matthews, Nicole L. Key
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Numerical Simulation of Surge in Axial Compressor
International Journal of Rotating Machinery, 2012 The object of this paper is to provide a reliable tool to simulate the stationary and transient operation performances in multistage axial compression systems, especially poststall behavior.
Wenhai Du, Olivier Léonard
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Robust design methodologies: application to compressor blades
, 2006 Compressor blades are subtle aerodynamic shapes designed after years of research and insight. They inevitably show deviations from their desired shapes due to manufacturing errors, erosion or foreign object damage.
Kumar, Apurva
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Axial compressor blades tip leakage flow control using natural aspiration. [PDF]
Sci Rep, 2023 Nejad PG, Zenouz RT.
europepmc +1 more source
Modification of axial-flow compressor stall margin by variation of stationary blade setting angles
, 1991 The useful operating range of the multistage, axial-flow compressor component of a gas turbine engine limits the extent of operation of that engine. Generally, the compressor stalls or surges at low flow rates and chokes at high flow rates.
Rukavina, John
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Performance Analysis of a Compressor Rotor Dedicated to Low-Power Drive Systems
EnergiesThis study investigates the efficiency evaluation of a compressor rotor designed for drive units requiring compressors with a power demand of less than 30 kW.
Natalia Kapela +2 more
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Techno-Economic Optimization of Multistage Membrane Processes with Innovative Hollow Fiber Modules for the Production of High-Purity CO2 and CH4 from Different Sources. [PDF]
Ind Eng Chem Res, 2022 Abejón R, Casado-Coterillo C, Garea A.
europepmc +1 more source