Solution to the binary diffusion laminar boundary-layer equations with second-order transverse curvature.
Author:
Affiliation:
1. Douglas Aircraft Company Inc., Long Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4252
Reference28 articles.
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1. Méthode de nachtsheim et swigert étendue à l'étude des couches limites laminaires bidimensionnelles planes ou axisymétriques non isothermes, avec effusion;International Journal of Heat and Mass Transfer;1996-08
2. Hypersonic interactions with surface mass transfer. I - Steady flow over a slender wedge wing;3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference;1982-06-07
3. Displacement-thickness induced pressures on a flat plate with homogeneous and heterogeneous vectored injection;International Journal of Heat and Mass Transfer;1980-03
4. Effective-Viscosity Model for Turbulent Wall Boundary Layers;Aeronautical Quarterly;1973-05
5. Boundary layer separation due to mass addition;Physics of Fluids;1973
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