Zobrazeno 1 - 10 of 13 pro vyhledávání: '"William R. Hawthorne"'
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Elektronická kniha
Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1
Autor: William R. Hawthorne
Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The
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3
Vote of thanks to Professor C. L. Wilson
Autor: William R. Hawthorne
Publikováno v: Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences. 358:136-139
I am sure you will all agree that the Fellowship of Engineering has made a good choice for its first lecture. The choice has been good in terms of the subject. Energy has always been important to engineers in this country and to the Royal Society. Ma
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::35c25636399cfec7afe0a3ac643c2023
https://doi.org/10.1098/rspa.1978.0002
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4
The effects of trailing vorticity on the flow through highly loaded cascades
Autor: James E. McCune, William R. Hawthorne
Publikováno v: Journal of Fluid Mechanics. 74:721-740
This paper presents a procedure whereby three-dimensional inviscid flow through a highly loaded turbomachinery cascade of lifting lines can be treated by methods corresponding to classical aerodynamic theory. In contrast to earlier linearized (thin a
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::12d02a8386640fa8d11df5b277bf6abd
https://doi.org/10.1017/s0022112076002024
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6
Secondary circulation in fluid flow
Autor: William R. Hawthorne
Publikováno v: Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences. 206:374-387
Secondary circulation appears after fluid with a non-uniform velocity distribution passes round a bend. It alters the character of the flow and is a source of loss. A general expression is developed for its change along a streamline in a perfect, inc
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::ccdfd17601d65ffc120c1824f4540dc8
https://doi.org/10.1098/rspa.1951.0076
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7
Some Exact Solutions of the Flow Through Annular Cascade Actuator Discs
Autor: Stephen L. Bragg, William R. Hawthorne
Publikováno v: Journal of the Aeronautical Sciences. 17:243-249
Exact solutions are presented for two types of flow of an incompressible inviscid fluid through an annular passage with a discontinuity in tangential velocity at one section, as would occur a t a cascade of airfoil blades of negligible chord. When st
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a4c79439f7200babf77e30d91f507ed2
https://doi.org/10.2514/8.1597
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