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Sail aerofoil applied to a vertical-axis wind turbineRobert, Jean. January 1977 (has links)
No description available.
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102 |
Modeling of combustion instabilities and their active control in a gas fueled combustorMohanraj, Rajendran 08 1900 (has links)
No description available.
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103 |
A study of heat release rate distribution in a gas turbine combustor by acoustic measurementsChao, Yei-Chin 05 1900 (has links)
No description available.
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104 |
Secondary flows in a rotating serpentine circular ductLaker, Travis S. 05 1900 (has links)
No description available.
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105 |
Design of a combustion chamber for an experimental gas turbineLyczko, Felix Joseph 12 1900 (has links)
No description available.
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106 |
Condensation in gas turbine inlet ductsFrey, David Alan 12 1900 (has links)
No description available.
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107 |
Performance of a viscous topping turbineCoons, Andrew Monroe 08 1900 (has links)
No description available.
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108 |
The effects of inlet water condensation on gas turbine performanceSkujins, Romans 08 1900 (has links)
No description available.
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109 |
Experimental investigation of the performance of a diffuser-augmented vertical axis wind turbineAkhgari, Arash 18 October 2011 (has links)
The performance of a vertical axis wind turbine with and without a diffuser was studied
using direct force measurement technique applied to a scaled model of the rotor in a
water tunnel. The experiment was conducted at different tip-speed ratios. The maximum
power coefficient for the turbine was found to be equal to 0.35 for the rotor with diffuser
and to 0.26 for the rotor without diffuser. Therefore, the maximum power coefficient was
increased by 35% when the diffuser was used in the configuration.
In the second part of this work, the flow patterns downstream of the turbine were
studied by the particle image velocimetry (PIV) technique. Six different tip-speed ratios
were considered for each configuration (with and without a diffuser). The vorticity and
the streamline plots provide insight into the flow physics in each configuration. In
addition, the swept area of a full-scale rotor was calculated for both a diffuser-augmented
and a bare turbine for a range of power outputs. / Graduate
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110 |
An improved treatment of two-dimensional two-phase flows of steam by a Runge-Kutta methodZamri, Mohd. Y. January 1997 (has links)
No description available.
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