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Herausgeber: 
  • National Aeronautics and Space Administr
    Autor(en): 
  • Rickey J. Shyne
  • Experimental Study of Boundary Layer Behavior in a Simulated Low Pressure Turbine 
     

    (Buch)
    Dieser Artikel gilt, aufgrund seiner Grösse, beim Versand als 2 Artikel!


    Übersicht

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    Lieferstatus:   i.d.R. innert 14-24 Tagen versandfertig
    Veröffentlichung:  März 2013  
    Genre:  Psychologie / Pädagogik 
    ISBN:  9781288915712 
    EAN-Code: 
    9781288915712 
    Verlag:  Creative Media Partners, LLC 
    Einband:  Kartoniert  
    Sprache:  English  
    Dimensionen:  H 246 mm / B 189 mm / D 9 mm 
    Gewicht:  308 gr 
    Seiten:  166 
    Bewertung: Titel bewerten / Meinung schreiben
    Inhalt:
    A detailed investigation of the flow physics occurring on the suction side of a simulated Low Pressure Turbine (LPT) blade was performed. A contoured upper wall was designed to simulate the pressure distribution of an actual LPT blade onto a flat plate. The experiments were carried out at Reynolds numbers of 100,000 and 250,000 with three levels of freestream turbulence. Freestream turbulence levels ranging from 0.8% to 3% was used in this experiment. Smoke-wire flow visualization data was used to confirm that the boundary layer was separated and formed a bubble. Hot-wires (single and x-wire) and surface mounted hot-film gases and static pressure taps were used to map the flowfield. The transition process over the separated flow region is observed to be similar to a laminar free shear layer flow with the formation of a large coherent eddy structure. For each condition, the locations defining the separation bubble were determined by careful examination of pressure and mean velocity profile data. Transition onset location and length determined from intermittency profiles decrease as freestream turbulence levels increase. Additionally, the length and height of the laminar separation bubbles were observed to be inversely proportional to the levels of freestream turbulence.

      



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