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Handbook of Turbomachinery Second Edition Revised - Ventech!

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volume will be equal to the accumulation rate in the control volume with<br />

time. In this general scheme the continuity, energy, and x-momentum<br />

equations to be solved on the grid are<br />

mass : SðrVx dAx þ rVy þ rVrdArÞ ¼<br />

energy : SðrVxhodAx þ rVyhodAy þ rVrhodArÞ ¼<br />

x momentum : SððP þ rV 2 xÞdAx ðDV=DtÞDr<br />

ðDV=DtÞDðrEÞ<br />

þ rVyVxdAy þ rVrVxdArÞ ¼DV=DtðDðrVxÞÞ<br />

Similar relationships govern the r-momentum and the moment <strong>of</strong><br />

momentum.<br />

There are many important details left unmentioned here on Denton’s<br />

method concerning the numerical solution technique, stability and damping,<br />

convergence, etc. These are available in the extensive literature on his<br />

method that Denton and his colleagues have published. Some other early<br />

developers <strong>of</strong> similar fully 3D methods deserving mention include Rai [23],<br />

Ni [24], and Ha [25]. Most <strong>of</strong> these follow the basic finite-volume, multigrid<br />

idea. For details on these methods, the reader is referred to the respective<br />

citations.<br />

CALCULATIONS AND MEASUREMENTS—FULLY 3D<br />

METHODS<br />

Figure 7shows asingle-stage, high rim speed, high-pressure turbine with a<br />

significant 3D design studied by Kingcombe et al. [26] at the Defense<br />

Equipment Research Agency (DERA) in the United Kingdom. The rigmeasured<br />

turbine aerodynamics were compared to the 3D Denton code. The<br />

vane drawing, Fig. 8, shows measured and computed isentropic Mach<br />

number pr<strong>of</strong>iles over the vane pressure surface. Agreement with the<br />

experiment is reasonably good, demonstrating the power <strong>of</strong> applying a<br />

true 3D code to the analysis <strong>of</strong> this very 3D geometry.<br />

For the heat transfer, Fig. 9gives the measured vane midspan heattransfer<br />

coefficient, expressed as Nu, taken from the vane cascade in<br />

DERA’s test facility. Also shown on the plot is a prediction using the<br />

Denton 3D Euler method and the STAN5 boundary-layer code incorporating<br />

the Van Driest damping function (see [11]), transition start length<br />

correlation by Seyb [27], and transition length correlation by Chen and<br />

Thyson [28]. (Note that contrary to usual custom, the suction side is on the<br />

left.) Kingcombe et al. state that the transition location and length were<br />

‘‘quite well’’ predicted although at some points the predictions and<br />

measurements were in better agreement than others. What is important is<br />

Copyright © 2003 Marcel Dekker, Inc.<br />

ð3Þ

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