The Unsteady Forces Due To Propeller-Appendage Interaction

1963 ◽  
Vol 30 (2) ◽  
pp. 279-287 ◽  
Author(s):  
O. Pinkus ◽  
J. R. Lurye ◽  
S. Karp

This paper presents a study of the nature of the unsteady forces in the field of a propeller rotating in the vicinity of an appendage. The propeller is assumed to be one of a high aspect ratio while the appendage, although of finite width, is assumed to be infinitely long, and thus the problem is reduced to a study of the unsteady flow field around two flat plates. An essential feature of the analysis is that the mutual interference effects of propeller blade and the appendage are taken into account. The method of solution employs the technique of the substitution vortex which yields explicit analytic expressions for the quasisteady, apparent-mass and wake forces for both the propeller and appendage. These equations provide the magnitude and variation of the total forces as functions of tip clearance, distance, and relative size of appendage and propeller.

2001 ◽  
Author(s):  
John Howell

Abstract Two approaches to increasing student retention and interest have been implemented in the undergraduate heat transfer course at The University of Texas at Austin. The first approach, under a Department-wide initiative in Project Based Education, is to assign a semester-long project that requires most of the basic material in the traditional heat transfer course to examine a practical engineering system. Three projects used to date will be briefly discussed. Second, a series of web-accessible interactive modules has been constructed. The objective is to develop intuitive understanding of phenomena generally taught in the undergraduate heat transfer course. These modules allow students to vary the important aspects of a problem and immediately see the result. For example, one module demonstrates the characteristics of fins added to a surface to improve heat loss. Envision the handle on a frying pan; the student can vary the handle material, the cooling of the handle by increasing air flow velocity over it, etc. and see the temperature that results along the handle length. Such effects are difficult to show with chalk and talk. The instructor may also use the modules in class with computer projection to demonstrate these effects. Nine modules have been developed to date. These demonstrate heat transfer by conduction through planar and cylindrical walls; heat transfer from materials with internal energy generation; fins; conduction in two-dimensional systems (under development); transient conduction in semi-infinite and finite-width slabs; convective heat transfer in flow over flat plates; convective heat transfer for flow in pipes; heat exchangers; and radiation in rectangular enclosures. Modules are programmed in JAVA for interactive use using any browser (Netscape or Explorer), and do not require a particular platform.


1999 ◽  
Vol 390 ◽  
pp. 1-23 ◽  
Author(s):  
OLIVIER BOULON ◽  
MATHIEU CALLENAERE ◽  
JEAN-PIERRE FRANC ◽  
JEAN-MARIE MICHEL

The present paper is devoted to an analysis of tip vortex cavitation under confined situations. The tip vortex is generated by a three-dimensional foil of elliptical planform, and the confinement is achieved by flat plates set perpendicular to the span, at an adjustable distance from the tip. In the range of variation of the boundary-layer thickness investigated, no significant interaction was observed between the tip vortex and the boundary layer which develops on the confinement plate. In particular, the cavitation inception index for tip vortex cavitation does not depend significantly upon the length of the plate upstream of the foil. On the contrary, tip clearance has a strong influence on the non-cavitating structure of the tip vortex and consequently on the inception of cavitation in its core. The tangential velocity profiles measured by a laser-Doppler velocimetry (LDV) technique through the vortex, between the suction and the pressure sides of the foil, are strongly asymmetric near the tip. They become more and more symmetric downstream and the confinement speeds up the symmetrization process. When the tip clearance is reduced to a few millimetres, the two extrema of the velocity profiles increase. This increase results in a decrease of the minimum pressure in the vortex centre and accounts for the smaller resistance to cavitation observed when tip clearance is reduced. For smaller values of tip clearance, a reduction of tip clearance induces on the contrary a significant reduction in the maxima of the tangential velocity together with a significant increase in the size of the vortex core estimated along the confinement plate. Hence, the resistance to cavitation is much higher for such small values of tip clearance and in practice, no tip vortex cavitation is observed for tip clearances below 1.5 mm. The cavitation number for the inception of tip vortex cavitation does not correlate satisfactorily with the lift coefficient, contrary to classical results obtained without any confinement. Owing to the specificity introduced by the confinement, the usual procedure developed in an infinite medium to estimate the vortex strength from LDV measurements is not applicable here. Hence, a new quantity homogeneous to a circulation had to be defined on the basis of the maximum tangential velocity and the core size, which proved to be better correlated to the cavitation inception data.


1992 ◽  
Vol 241 ◽  
pp. 261-289 ◽  
Author(s):  
N. Peake

The ingestion of convected vorticity by a high-solidity rotating blade row is a potent noise source in modern aeroengines, due largely to the high level of mutual aerodynamic interactions between adjacent blades. In order to model this process we solve the problem of determining the unsteady lift on an infinite cascade of finite-chord flat plates due to an incident vorticity wave. The method of solution is the Wiener–Hopf technique, and we consider the case of the reduced frequency, Ω, being large, allowing application of asymptotic analysis in the formal limit Ω → ∞. This approach yields considerable simplification, both in allowing the truncation of an infinite reflection series to just two terms, and in allowing algebraic expressions for the Wiener–Hopf split functions to be found. The unsteady lift distribution is derived in closed form, and the accuracy of the asymptotic Wiener–Hopf factorization demonstrated for even modest values of Ω by comparison with exact (but less tractable) methods. Our formulae can easily be incorporated into existing noise prediction codes: the advantage of our scheme is that it handles a regime in which conventional numerical approaches become unwieldy, as well as providing significant physical insight into the underlying mechanisms.


Author(s):  
Stefania De Curtis ◽  
Daniele Dominici

AbstractSpin-1 resonances are naturally present in composite Higgs frameworks. We first review a model independent approach to parameterize a single additional heavy triplet and then we consider more realistic models arising in composite Higgs scenarios where a larger number of spin-1 resonances is expected. In these cases, finite width and interference effects can heavily affect the bounds extracted from the data.


Author(s):  
Yushin Ehara ◽  
Soichiro Kitamura ◽  
Wakana Tsuru ◽  
Satoshi Watanabe ◽  
Shin-Ichi Tsuda

Author(s):  
Bart van Esch ◽  
Li Cheng

Many mixed-flow and axial flow pumps exhibit a so-called unstable head curve. Due to the risk of instabilities this flow region is usually avoided during pump operation. This paper presents experimental and numerical research on the relation between the instability in the head curve and the magnitude of unsteady hydraulic forces. It is found that there is a strong influence of the extend of the clearance gap between impeller blades and casing. The spectral content of the forces shows evidence of rotating instabilities. It indicates that not only instability of the head curve and unsteady forces are interrelated, but also rotating instabilities play a role in this phenomenon. Results of CFD calculations are presented as well, showing the difficulties in simulating the flow under such conditions.


1976 ◽  
Vol 43 (4) ◽  
pp. 567-570 ◽  
Author(s):  
M. Shafir ◽  
S. G. Rubin

Turbulent boundary-layer behavior in the vicinity of a right-angle corner formed by intersecting flat plates is considered. Due to interference effects a secondary flow is induced. Numerical solutions are obtained for the main stream and secondary motion. Models with and without intermittency factors are considered. It is shown that the secondary motion is significantly different for laminar and turbulent conditions. Similar behavior has previously been observed experimentally.


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