Computed Effect of Varying Tip Clearance and Axial Gap on Gas turbine Stage Performance Part (I): (Steady Flow)

Faculty Engineering Year: 2016
Type of Publication: ZU Hosted Pages:
Authors:
Wael Mohamed Olwan Farahat
Journal: المجلة المصرية الدولية للعلوم الهندسية والتكنولوجيا جامعة الزقازيق Volume:
Keywords : Computed Effect , Varying , Clearance , Axial , , , turbine    
Abstract:
In the present work, the effect of tip clearance on turbine performance is numerically investigated. This is carried out by studying the clearance ratio effect (the ratio between the clearance height and the blade height) at values of 2.4%,
    
     
 
       

Author Related Publications

  • Wael Mohamed Olwan Farahat, "EFFECTS OF VARYING TIP CLEARANCE AND AXIAL GAP ON AXIAL-FLOW TURBINE STAGE PERFORMANCE ( PRESENT STATE OF THE ART)", جامعة الزقازيق, 2015 More
  • Wael Mohamed Olwan Farahat, "Thermal performance augmentation of a semi-circular cylinder in crossflow using longitudinal fins", Elsevier, 2021 More

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