An Improved Streamline Curvature Approach for Off-Design Analysis of Transonic Compression Systems by Keith M. Boyer Dissertation submitted to the Faculty of the Virginia Polytechnic Institute and State University in partial fulfillment of the requirements for the Degree of Doctor of Philosophy in Mechanical Engineering Graduate Committee Walter F. O’Brien, Chairman Peter S. King Wing F. Ng.
This Report describes a computer program for the analysis of the fluid motion in the meridional plane of axial flow turbomachines. The method uses a streamline curvature approach and the program allows calculations within blade rows. Comparisons with experiment and various other methods of analysis are presented. LIST OF CONTENTS 1.This paper describes a newly developed streamline curvature throughflow method for the analysis of radial or mixed flow machines. The code includes curved walls, curved leading and trailing edges.A streamline curvature throughflow numerical approach is assessed and modified to better approximate the flow fields of transonic axial compression systems. Improvements in total pressure loss modeling are implemented, central to which is a physics-based shock model, to ensure accurate and reliable off-design performance prediction. The new model accounts for shock geometry changes, with shock.
A streamline curvature method works only good, if you have good loss correlations. Up until now, no loss correlations were implemented. We have done an more or less extensive literature research of loss correlations. So it would be an option for your students, to implement some of these correlations int the skv. I would be really interested in that! If you want to start development, I suggest.
A streamline curvature (SLC) throughflow numerical model was assessed and modified to better approximate the flow fields of highly transonic fans typical of military fighter applications. Specifically, improvements in total pressure loss modeling were implemented to ensure accurate and reliable off-design performance prediction. The assessment was made relative to the modeling of key transonic.
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A STREAMLINE CURVATURE METHOD FOR DESIGN OF SUPERCRITICAL AND SUBCRITICAL AIRFOILS By Raymond L. Barger and Cuyler W. Brooks, Jr. Langley Research Center SUMMARY An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described. The method is based on the streamline curvature velocity equation. Sev-.
The relationship between streamline curvature and bed resistance in shallow water flow with little side constraint, as derived in 1970 by H.J. Schoemaker, is reconsidered. Schoemaker concluded that the bed resistance causes the curvature of a free streamline to grow exponentially with the distance along this streamline, thus giving rise to a destabilizing tendency. The present analysis shows.
The effect of streamline curvature on turbulence is a well established phenomenon and numerous literature (Bradshaw, Moser et al., Holloway et al. ) are available describing the effect of streamline curvature on turbulence for the wall bounded flows.
Equation of Motion in Streamline Coordinates Ain A. Sonin, MIT. 2.25 Advanced Fluid Mechanics. Euler’s equation expresses the relationship between the velocity and the pressure fields in inviscid flow. Written in terms of streamline coordinates, this equation gives information about not only about the pressure-velocity relationship along a streamline (Bernoulli’s equation), but also.
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Streamline curvature in the plane of the mean shear produces large changes in the turbulence structure of shear layers, usually an order of magnitude more important than normal pressure gradients and other terms in the mean-motion equations for curved flows. The effects on momentum and heat transfer in boundary layers are noticeable on typical wing sections and are very important on highly.