... | ... | @@ -6,68 +6,16 @@ The main parameters of the present database of are given in the below table. |
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The parameters used in this database are defined with free stream conditions.
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`<table border="1" class="colwidths-given docutils align-center">
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<colgroup>
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<col width="20%" />
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<col width="80%" />
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</colgroup>
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<tbody valign="top">
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<tr class="row-odd"><td>Displacement thicknesses (based on the velocity at the boundary layer edge):</td>
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<td><span class="math">\(\displaystyle \delta^{*}_s = \int_0^\delta (1-\frac{\rho}{\rho_\delta}\frac{V_s}{V_\delta}) ds\)</span> (deltas),
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<span class="math">\(\displaystyle \delta^{*}_n = -\int_0^\delta (1-\frac{\rho}{\rho_\delta}\frac{V_n}{V_\delta}) ds\)</span> (deltan)</td>
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</tr>
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<tr class="row-even"><td>Momentum thicknesses:</td>
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<td><span class="math">\(\displaystyle \theta_{ss} = \int_0^\delta \frac{\rho}{\rho_\delta}\frac{V_s}{V_\delta}(1-\frac{V_s}{V_\delta}) ds\)</span> (thetass),
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<span class="math">\(\displaystyle \theta_{nn} = \int_0^\delta \frac{\rho}{\rho_\delta}\frac{V_n}{V_\delta}(1-\frac{V_n}{V_\delta}) ds\)</span> (thetann)</td>
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</tr>
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<tr class="row-odd"><td>Kinetic energy thicknesses:</td>
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<td><span class="math">\(\displaystyle \theta_{es} = \int_0^\delta \frac{\rho}{\rho_\delta}\frac{V_s}{V_\delta}(1-\frac{V_s^2}{V_\delta^2}) ds\)</span> (deltaes),
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<span class="math">\(\displaystyle \theta_{en} = \int_0^\delta \frac{\rho}{\rho_\delta}\frac{V_n}{V_\delta}(1-\frac{V_n^2}{V_\delta^2}) ds\)</span> (deltaen)</td>
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</tr>
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<tr class="row-even"><td>Shape factors:</td>
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<td><span class="math">\(\displaystyle H12 = \frac{\delta^{*}_s}{\theta_{ss}}\)</span>,
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<span class="math">\(\displaystyle H22 = \frac{\delta^{*}_n}{\theta_{nn}}\)</span></td>
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</tr>
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<tr class="row-odd"><td>Pressure coefficients:</td>
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<td><span class="math">\(\displaystyle Cp = \frac{p - p_{\infty}}{\frac{1}{2}\rho_{\infty} V_{\infty}^2}\)</span> (cp_static),
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<span class="math">\(\displaystyle Kp = \frac{p_{tot} - p_{\infty}}{\frac{1}{2}\rho_{\infty} V_{\infty}^2}\)</span> (cp_dyn)</td>
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</tr>
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<tr class="row-even"><td>Skin friction coefficients:</td>
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<td><span class="math">\(\displaystyle Cf_{\delta} = (\mu_w + \mu_t) \frac{{\frac{\partial V}{\partial w}}_{|_w}}{\frac{1}{2}\rho_w V_\delta^2}\)</span>,
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<span class="math">\(\displaystyle Cf_{\infty} = (\mu_w + \mu_t) \frac{{\frac{\partial V}{\partial w}}_{|_w}}{\frac{1}{2}\rho_\infty V_\infty^2}\)</span></td>
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</tr>
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<tr class="row-odd"><td> </td>
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<td><span class="math">\(\displaystyle Y^+ = Y \frac{V^\star}{\nu}\)</span></td>
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</tr>
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<tr class="row-even"><td>Velocity normalized by the shear stress velocity:</td>
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<td><span class="math">\(\displaystyle V^+ = \frac{V}{V^\star}\)</span></td>
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</tr>
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<tr class="row-odd"><td>Shear stress at the wall:</td>
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<td><span class="math">\(\displaystyle \tau_w = \mu_w \frac{\partial u}{\partial y}\)</span></td>
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</tr>
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<tr class="row-even"><td>Shear stress velocity (friction velocity) at the wall:</td>
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<td><span class="math">\(\displaystyle V^\star = \sqrt{\frac{\tau_w}{\rho_w}}\)</span></td>
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</tr>
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<tr class="row-odd"><td>Total pressure loss:</td>
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<td><span class="math">\(\displaystyle \frac{\Delta P_t}{P_t} = \frac{P_t - {P_t}_\infty}{{P_t}_\infty}\)</span> (PtotLoss)</td>
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</tr>
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<tr class="row-even"><td>Skew angles:</td>
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<td><span class="math">\(\displaystyle \beta = \gamma - \gamma_\delta\)</span>,
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<span class="math">\(\displaystyle \beta_w = \gamma_w - \gamma_\delta\)</span></td>
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</tr>
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</tbody>
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</table>`
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## WP 1.1
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## $`\mathcal{C}_1`$
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- Wall pressure data
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- [Aerodynamic data](/../tree/master/DATA/AerodynamicData/wp11)
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- [Boundary Layer quantities](/../tree/master/DATA/AerodynamicData/wp11)
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## WP 1.2
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- Wall pressure data
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- [Aerodynamic data](https://gitlab.com/jbodart/scone/-/tree/master/DATA/AerodynamicData/wp12)
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- [Boundary Layer quantities(https://gitlab.com/jbodart/scone/-/tree/master/DATA/AerodynamicData/wp12)
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## WP 2.2 |
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\ No newline at end of file |