Results 21 to 30 of about 10,638 (359)
Time-domain harmonic balance method for aerodynamic and aeroelastic simulations of turbomachinery flows [PDF]
, 2013 A time-domain Harmonic Balance method is applied to simulate the blade row interactions and vibrations of state- of-the-art industrial turbomachinery configurations. The present harmonic balance approach is a time-integration scheme that turns a periodic
Besicovitch A.S. +5 more
core +1 more source
Advanced Compressor Loss Correlations, Part I: Theoretical Aspects
International Journal of Rotating Machinery, 1997 Reliable efficiency calculation of high-subsonic and transonic compressor stages requires a detailed and accurate prediction of the flow field within these stages.
M. T. Schobeiri
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Inlet Flow Angle Determination of Transonic Compressor Cascades [PDF]
Journal of Turbomachinery, 1991 Tests of transonic compressor cascades require special measuring techniques to determine the inlet flow angle around sonic inlet flow conditions. One of the main requirements for these methods is the ability to adjust the inlet flow angle during the test to a prescribed value.
Steinert, W., Fuchs, R., Starken, H.
openaire +3 more sources
Engineering Applications of Computational Fluid Mechanics, 2021 Design optimization of transonic airfoils for rotary blades is a challenging subject that remarkably affects the stage and overall performance of axial-flow compressors.
A. Zeinalzadeh, M.R. Pakatchian
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State-of-Art of Transonic Axial Compressors [PDF]
, 2011 Transonic axial flow compressors are today widely used in aircraft engines to obtain maximum pressure ratios per single-stage. High stage pressure ratios are important because they make it possible to reduce the engine weight and size and, therefore, investment and operational costs.
Biollo Roberto, BENINI, ERNESTO
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Advances in Mechanical Engineering, 2017 Numerical simulation has been conducted on a transonic contra-rotating axial compressor to investigate the shock wave and flow characteristics under various operation conditions.
Hanru Liu +3 more
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A New Method for Rapid Optimization Design of a Subsonic Tandem Blade
Applied Sciences, 2020 Tandem blade technology has been developed for years due to its capacity to bear higher aerodynamics than conventional configurations. Even so, there is still the tough problem of how to design tandem blades effectively and further improve blade ...
Yuan Tao, Xianjun Yu, Baojie Liu
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Aerostructural Optimization of a Transonic Compressor Rotor [PDF]
Journal of Propulsion and Power, 2006 This paper presents a framework for multi-objective and multidisciplinary design optimization using highfidelity analysis tools. In this framework the aerodynamic performance is evaluated based on a Navier‐Stokes equation solver, and the structure dynamics is computed using commercially available finite element software.
Lian, Yongsheng, Liou, Meng-Sing
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Numerical Simulation of Transonic Compressors with Different Turbulence Models
Aerospace, 2023 One of the most commonly used techniques in aerospace engineering is the RANS (Reynolds average Navier–Stokes) approach for calculating the transonic compressor flow field, where the accuracy of the computation is significantly affected by the turbulence
Wenhui Yan +6 more
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Test Facility for High-Speed Probe Calibration [PDF]
EPJ Web of Conferences, 2019 A new test facility was built up as a part of a closed-loop transonic wind tunnel in VZLU´s High-speed Aerodynamics Department. The wind tunnel is driven by a twelve stage radial compressor and Mach and Reynolds numbers can be changed by the compressor ...
Jelínek Tomáš +3 more
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