First-Order Slip Effects on the Compressible Laminar Boundary Layer Over a Slender Body of Revolution in Axial Flow
1961; American Institute of Aeronautics and Astronautics; Volume: 28; Issue: 6 Linguagem: Inglês
10.2514/8.9057
ISSN1936-9999
Autores Tópico(s)Gas Dynamics and Kinetic Theory
Resumo* Former ly , Resea rch Ass is tant , D e p a r t m e n t of Aeronau t i ca l Engineer ing , Univers i ty of M a r y l a n d . MANY FIRST-ORDER SLIP ANALYSES have been performed for boundary layers neglecting transverse curvature. I t is the purpose of this note to examine the compressible boundary layer with transverse curvature in first-order slip flow. Correct to the first-order in slip, the continuum boundary-layer equations with first-order slip and jump boundary conditions are applicable. The present analysis extends the continuum analysis of Probstein and Elliott to include first-order slip. The Busemann and Crocco integrals are also discussed. No boundarylayer interaction effects are considered and only the zero pressure-gradient case is examined, f The axial symmetric laminar boundary-layer equations for a perfect gas with constant Prandtl number and specific heats in first-order slip flow are the same as the continuum equations given in reference 1 [see Eqs. (4)-(7) of reference 1]. The continuum boundary conditions, lim u(x, y) = ue(x)t, v(xt 0) = 0, y—>• oo
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