M
Mukka Govardhan
Researcher at Indian Institute of Technology Madras
Publications - 57
Citations - 481
Mukka Govardhan is an academic researcher from Indian Institute of Technology Madras. The author has contributed to research in topics: Axial compressor & Tip clearance. The author has an hindex of 12, co-authored 57 publications receiving 415 citations. Previous affiliations of Mukka Govardhan include Universiti Malaysia Sabah.
Papers
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Computational analysis of performance and flow investigation on wells turbine for wave energy conversion
TL;DR: In this article, the performance and aerodynamic analysis of the NACA 0021 constant chord blades of the Wells turbine with different flow coefficients were analyzed and the model was used to predict the turbine stall rate and the flow coefficient at which the turbine stalls.
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Influence of fillet shapes on secondary flow field in a transonic axial flow turbine stage
TL;DR: In this paper, the effect of leading edge modifications via fillet shapes near vane/blade-endwall juncture in a transonic environment within the highly loaded high pressure turbine stage was investigated.
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Secondary Flow Loss Reduction in a Turbine Cascade with a Linearly Varied Height Streamwise Endwall Fence
Krishna N. Kumar,Mukka Govardhan +1 more
TL;DR: In this paper, the authors proposed a streamwise endwall fence to reduce secondary flow losses by application of end-wall fence, which is the optimum fence for secondary flow loss reduction.
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Effect of guide vanes on the performance of a self-rectifying air turbine with constant and variable chord rotors
TL;DR: In this paper, an experimental investigation was carried out on a Wells turbine with the constant chord and variable chord blade rotors fitted with inlet and outlet guide vanes to understand the aerodynamics.
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Computational study of the effect of sweep on the performance and flow field in an axial flow compressor rotor
TL;DR: In this paper, the performance and three-dimensional flow pattern within and at the exit of swept and unswept rotors were analyzed with a specific intention of understanding the threedimensional flow patterns within the rotors and also the pattern of the blade boundary layer flow.