NASA NTRS · 19740000129
Computer program for calculating laminar, transitional, and turbulent boundary layers for a compressible axisymmetric flow
Abstract
Finite-difference computer program calculates viscous compressible boundary layer flow over either planar or axisymmetric surfaces. Flow may be initially laminar and progress through transitional zone to fully turbulent flow, or it may remain laminar, depending on imposed boundary conditions, laws of viscosity, and numerical solution of momentum and energy equations.
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Albers, J. A., Gregg, J. L.. 1974-12-01. Computer program for calculating laminar, transitional, and turbulent boundary layers for a compressible axisymmetric flow. https://ntrs.nasa.gov/citations/19740000129
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