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St Stanton number

Fig. 19. Kays MTEN calculation for the heat transfer to an accelerating boundary layer (St = Stanton number). Fig. 19. Kays MTEN calculation for the heat transfer to an accelerating boundary layer (St = Stanton number).
Re vibrational Reynolds number = 2natD /v s lateral spacing between strip fins m, ft St Stanton number = h/Gc = Nu/Re Pr Sw Swirl flow parameter Sw = Re, ,Vy T temperature °C, °F... [Pg.843]

Nu Nusselt number Pr Prandtl number Re Reynolds number St Stanton number... [Pg.190]

St = Stanton number for transfer across capillary wall... [Pg.155]

See other pages where St Stanton number is mentioned: [Pg.287]    [Pg.94]    [Pg.737]    [Pg.663]    [Pg.789]    [Pg.236]    [Pg.284]    [Pg.194]    [Pg.212]    [Pg.254]    [Pg.295]    [Pg.238]    [Pg.252]    [Pg.663]    [Pg.786]    [Pg.262]    [Pg.479]    [Pg.382]    [Pg.1266]    [Pg.1266]    [Pg.81]    [Pg.52]    [Pg.779]    [Pg.1393]    [Pg.1466]    [Pg.539]    [Pg.91]    [Pg.659]    [Pg.737]    [Pg.1]    [Pg.93]    [Pg.158]    [Pg.287]    [Pg.953]    [Pg.122]    [Pg.70]    [Pg.275]    [Pg.352]    [Pg.73]    [Pg.110]    [Pg.97]    [Pg.436]    [Pg.96]    [Pg.122]    [Pg.110]   
See also in sourсe #XX -- [ Pg.3 ]



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Stanton

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