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Axial compressor

About: Axial compressor is a research topic. Over the lifetime, 12035 publications have been published within this topic receiving 127766 citations.


Papers
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Journal ArticleDOI
TL;DR: In this paper, a 32MW gas turbine experienced a severe failure accompanied by a loud noise near its second natural frequency at 4200rpm, and all of the stationary and rotary blades of stages 14-18 of the compressor had been detached from the dovetail region of the disks.

52 citations

Journal ArticleDOI
TL;DR: In this paper, the vibration behavior of a flexible cylinder subjected to an axial flow is investigated numerically and a methodology is constructed, which relies entirely on fluid-structure interaction calculations.

52 citations

Journal ArticleDOI
TL;DR: In this article, a linear analysis of the ideal magnetohydrodynamic stability of the Z-pinch is presented in which plasma flows are included in the equilibrium, and it is shown that substantial stabilization of internal modes is possible for some equilibrium profiles.
Abstract: A linear analysis of the ideal magnetohydrodynamic (MHD) stability of the Z‐pinch is presented in which plasma flows are included in the equilibrium. With sheared axial flows it is found that substantial stabilization of internal modes is possible for some equilibrium profiles. For this to occur equilibria with a change in fluid velocity across the pinch radius of about Mach 2 are required. However, this ignores the surrounding vacuum and for the more realistic free boundary modes flows of about Mach 4 are required to stabilize all global MHD modes. This stabilization of MHD modes is not observed for all equilibria however. This fact, combined with the supersonic flow speeds required for stability, make it unlikely that a Z‐pinch could in practice be stabilized by the introduction of sheared flow.

52 citations

Patent
19 Feb 1975
TL;DR: In this paper, a windmill having thermal and electric power output and including windmill blades rotatably mounted and connected to a speed increaser mechanism of gears and shafts was shown.
Abstract: A windmill having thermal and electric power output and including windmill blades rotatably mounted and connected to a speed increaser mechanism of gears and shafts and a centrifugal compressor connected to the windmill thru the speed increaser to be driven by virtue of the wind applied to the blades of the windmill itself A directional control is connected to the windmill head to have the windmill blades face into the wind, as desired The compressor is connected to an insulated heat storage tank which contains storage material, such as brick, and the compressor discharge velocity and pressure difference are converted to heat, and the compressor fluid is returned to the compressor thru a screen which protects the compressor, and there is a flow control which automatically compensates for changes in density of the circulated air or compressor fluid Also, a gas turbine generator can be connected with the compressor to be driven thereby, and electric elements could be connected with the generator for producing electricity Two other embodiments show an impeller type of air brake and a valve and a heat-sensitive control, for generating heat or power

52 citations

Journal ArticleDOI
01 Mar 2003
TL;DR: In this article, a transonic compressor rotor (NASA rotor 37) using the response surface method (RSM) and three-dimensional Navier-Stokes analysis has been carried out in this work.
Abstract: Design optimization of a transonic compressor rotor (NASA rotor 37) using the response surface method (RSM) and three-dimensional Navier-Stokes analysis has been carried out in this work. The Baldwin—Lomax turbulence model was used in the flow analysis. Three design variables were selected to optimize the stacking line of the blade. Data points for response evaluations were selected by D-optimal i design, and a linear programming method was used to optimize the response surface. As a main result of the optimization, adiabatic efficiency was successfully improved. It was found that the optimization process provides reliable design of a turbomachinery blade with reasonable computing time.

52 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202398
2022304
2021217
2020288
2019316
2018353