Abstract
In this chapter, the author’s zonal, spectral solutions for the partial differential equations (PDE) of the three-dimensional stationary, compressible boundary layer (CBL) given as in [1]–[3] for the computation of the flow over flattened, flying configurations (FC) are now extended to the Navier-Stokes layer (NSL). If \( \eta = \left( {{x_3} - Z\left( {{x_1},{x_2}} \right)} \right)/\delta \left( {{x_1},{x_2}} \right) \) is a new coordinate, the spectral forms of the axial, lateral, and vertical velocity components \( {u_{\delta }},{v_{\delta }}, and w\delta \), of the density function \( R = \ln \rho \) and of the absolute temperature T (31.1)—(31.5) and their nine boundary conditions (31.6)-(31.14), at the NSL-edge \( \left( {\eta = 1} \right) \), are
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References
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Nastase, A. (2002). Comparison of Zonal, Spectral Solutions for Compressible Boundary Layer and Navier—Stokes Equations. In: Constanda, C., Schiavone, P., Mioduchowski, A. (eds) Integral Methods in Science and Engineering. Birkhäuser, Boston, MA. https://doi.org/10.1007/978-1-4612-0111-3_31
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DOI: https://doi.org/10.1007/978-1-4612-0111-3_31
Publisher Name: Birkhäuser, Boston, MA
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