Vanamala Ushasri’s scientific contributions

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Publications (1)

Figure 1. Three dimensional view of the centrifugal impeller.
Figure 2. Computational domain of single passage.
Figure 3. Passage grid block structure near leading edge at blade mid span.
Figure 7. Mass averaged static pressure rise coefficient across the exit of the impeller with different blade tip chamfers at R=1.016, τ=2%.
Figure 8. Contours of total pressure coefficient at radial location R=0.984, τ=2%, φ=0.42.

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Computational Investigation of Flow in a Centrifugal Impeller with Chamfered Blade Tips: Effects of Stage Loading and Tip Clearance
  • Article
  • Full-text available

August 2020

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242 Reads

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1 Citation

International Journal of Fluid Mechanics & Thermal Sciences

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Vanamala Ushasri
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