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κ,,n,,=,,∫,,0,,∞,,(,,y,,−,,δ,,∗,,),,n,,d,,u,,(,,y,,),,/,,u,,0,,d,,y,,d,,y,,{displaystyle,,{kappa,,{n}}=int,,{0}^{infty,,}{(y-{delta,,^{*}})^{n}{du(y)/u{0},,over,,dy}mathrm,,{d},,y}},,Princeton,,,,University,,,,Press,,,,,1996The,,,,velocity,,,,thickness,,,,can,,,,also,,,,be,,,,referred,,,,to,,,,as,,,,the,,,,Soole,,,,ratio,,,,,although,,,,the,,,,gradient,,,,of,,,,the,,,,thickness,,,,over,,,,distance,,,,would,,,,be,,,,adversely,,,,proportional,,,,to,,,,that,,,,of,,,,velocity,,,,thicknessContents,,,,1,,,,99%,,,,Boundary,,,,Layer,,,,thickness,,,,2,,,,Displacement,,,,thickness,,,,3,,,,Momentum,,,,thickness,,,,4,,,,Energy,,,,thickness,,,,5,,,,Shape,,,,factor,,,,6,,,,Moment,,,,Method,,,,7,,,,Further,,,,reading,,,,8,,,,Notes,,,,9,,,,References,,,,Laminar,,,,flow,,,,theory141There,,are,,some,,advantages,,to,,also,,include,,descriptions,,of,,moments,,of,,the,,boundary,,layer,,profile,,derivatives,,with,,respect,,to,,the,,height,,above,,the,,wallConsider,,,a,,,stationary,,,body,,,with,,,a,,,fluid,,,flowing,,,around,,,it,,,,like,,,the,,,semi-infinite,,,flat,,,plate,,,with,,,air,,,flowing,,,over,,,the,,,top,,,of,,,the,,,plate,,,(assume,,,the,,,flow,,,and,,,the,,,plate,,,extends,,,to,,,infinity,,,in,,,the,,,positive/negative,,,direction,,,perpendicular,,,to,,,the,,,x,,,−,,,y,,,{displaystyle,,,x-y},,,plane)141The,,,,higher,,,,the,,,,value,,,,of,,,,H,,,,,the,,,,stronger,,,,the,,,,adverse,,,,pressure,,,,gradientA,,,,shape,,,,factor,,,,is,,,,used,,,,in,,,,boundary,,,,layer,,,,flow,,,,to,,,,determine,,,,the,,,,nature,,,,of,,,,the,,,,flowThe,,,velocity,,,profiles,,,central,,,moments,,,are,,,defined,,,as:^,,Schlichting,,,pWhere,,,ρ,,,0,,,{displaystyle,,,rho,,,{0}},,,and,,,u,,,0,,,{displaystyle,,,u{0}},,,are,,,the,,,density,,,and,,,velocity,,,in,,,the,,,'free,,,stream',,,outside,,,the,,,boundary,,,layer,,,,and,,,y,,,{displaystyle,,,y},,,is,,,the,,,coordinate,,,normal,,,to,,,the,,,wallζ,,,,n,,,,=,,,,∫,,,,0,,,,∞,,,,(,,,,y,,,,−,,,,m,,,,),,,,n,,,,1,,,,δ,,,,∗,,,,(,,,,1,,,,−,,,,u,,,,(,,,,y,,,,),,,,u,,,,0,,,,),,,,d,,,,y,,,,{displaystyle,,,,{zeta,,,,{n}}=int,,,,{0}^{infty,,,,}{(y-m)^{n}{1,,,,over,,,,delta,,,,^{*}}(1-{u(y),,,,over,,,,u{0}})mathrm,,,,{d},,,,y}},,,,The,,,,definition,,,,for,,,,incompressible,,,,flow,,,,can,,,,be,,,,based,,,,on,,,,volumetric,,,,flow,,,,rate,,,,,as,,,,the,,,,density,,,,is,,,,constant:where,,,the,,,mean,,,location,,,is,,,the,,,displacement,,,thickness,,,δ,,,∗,,,{displaystyle,,,delta,,,^{*}},,,638γ,,,,1,,,,=,,,,κ,,,,3,,,,/,,,,κ,,,,2,,,,3,,,,/,,,,2,,,,=,,,,(,,,,2,,,,δ,,,,∗,,,,3,,,,−,,,,6,,,,δ,,,,∗,,,,α,,,,1,,,,+,,,,3,,,,α,,,,3,,,,),,,,/,,,,(,,,,−,,,,δ,,,,∗,,,,2,,,,+,,,,2,,,,α,,,,1,,,,),,,,3,,,,/,,,,2,,,,{displaystyle,,,,gamma,,,,{1}=kappa,,,,{3}/kappa,,,,{2}^{3/2}=(2delta,,,,^{*3}-6delta,,,,^{*}alpha,,,,{1}+3alpha,,,,{3})/(-delta,,,,^{*2}+2alpha,,,,{1})^{3/2}},,,,Boundary-Layer,,,,Theory,,,,,7th,,,,ed.,,,,,McGraw,,,,Hill,,,,,New,,,,York,,,,,U.S.AFor,,,,laminar,,,,boundary,,,,layers,,,,over,,,,a,,,,flat,,,,plate,,,,,the,,,,Blasius,,,,solution,,,,to,,,,the,,,,flow,,,,governing,,,,equations,,,,gives:[1]In,,the,,equations,,above,,,ρ,,0,,{displaystyle,,rho,,{0}},,and,,u,,0,,{displaystyle,,u{0}},,are,,therefore,,replaced,,with,,ρ,,e,,{displaystyle,,rho,,{e}},,and,,u,,e,,{displaystyle,,u{e}},,A,,high,,adverse,,pressure,,gradient,,can,,greatly,,reduce,,the,,Reynolds,,number,,at,,which,,transition,,into,,turbulence,,may,,occurIn,,,,the,,,,equations,,,,above,,,,,ρ,,,,0,,,,{displaystyle,,,,rho,,,,{0}},,,,and,,,,u,,,,0,,,,{displaystyle,,,,u{0}},,,,are,,,,therefore,,,,replaced,,,,with,,,,ρ,,,,e,,,,{displaystyle,,,,rho,,,,{e}},,,,and,,,,u,,,,e,,,,{displaystyle,,,,u{e}},,,,99%,,Boundary,,Layer,,thickness[edit]Where,,ρ,,0,,{displaystyle,,rho,,{0}},,and,,u,,0,,{displaystyle,,u{0}},,are,,the,,density,,and,,velocity,,in,,the,,'free,,stream',,outside,,the,,boundary,,layer,,,and,,y,,{displaystyle,,y},,is,,the,,coordinate,,normal,,to,,the,,wallwhere,,,,H,,,,is,,,,the,,,,shape,,,,factor,,,,,δ,,,,∗,,,,{displaystyle,,,,delta,,,,^{*}},,,,is,,,,the,,,,displacement,,,,thickness,,,,and,,,,,,,,is,,,,the,,,,momentum,,,,thicknessFurther,,,,reading[edit]^,,Weyburne,,,2014δ,,,3,,,=,,,∫,,,0,,,∞,,,u,,,(,,,y,,,),,,u,,,o,,,(,,,1,,,−,,,u,,,(,,,y,,,),,,2,,,u,,,o,,,2,,,),,,d,,,y,,,{displaystyle,,,delta,,,{3}=int,,,{0}^{infty,,,}{{u(y),,,over,,,u{o}}{left(1-{u(y)^{2},,,over,,,u{o}^{2}}right)}},mathrm,,,{d},,,y},,, bcfaf6891f

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