Jak kupować
Dostawa
Doradca ds. zakupów
Flow Separation Prevention on a Turbine Blade in Cascade at Low Reynolds Number
Angielski
150 b
30 dni na zwrot towaru
Mogłoby Cię także zainteresować
/
Miękka
88.05
zł
/
Twarda
94.63
zł
/
Miękka
67.51
zł
The problem of flow separation from a low pressure turbine blade was investigated. The operating conditions under which the separation occurred were documented through measurement of surface pressure coefficients, boundary layer velocity and turbulence profiles, total pressure loss coefficient and wake velocity momentum deficit. Three different means for reducing the losses associated with the flow separation were also investigated. A boundary layer trip, dimples, and V -grooves were studied as passive means requiring no additional energy to reduce the separation losses. The boundary layer trip was only successful for an inlet and axial chord Reynolds number of 50k with a reduction in loss coefficient of 58.2%. Three sets of dimples were tested with the placement of each at axial chord locations of 50%, 55%, and 65%.
Informacje o książce
Angielski
Kategoria
