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Project TitleSTAN5
Track CodeLEW-13009
DescriptionThis computer program was developed to compute general two-dimensional turbulent boundary layer flow using finite difference techniques. STAN 5 has gone through a considerable period of development and has proved accurate and useful in experimental turbulent boundary layer research at Stanford University. STAN 5 is able to handle a large variety of boundary layer problems without requiring any modifications to the program code including boundary layers on a flat plate, flow inside nozzles and diffusers (for a prescribed potential flow distribution), flow over axisymmetric bodies, and developing and fully developed flow inside circular pipes and flat ducts. The flows may be laminar or turbulent, and provision is made to handle transition.
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