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Airfoil Design for a Prescribed Velocity Distribution in Transonic Flow by an Integral MethodIn the present paper a method for the design of airfoils for a prescribed transonic contour velocity distribution is developed. It applies the fundamental ideas of the integral method after K. Oswatitsch for the prediction of the velocity distribution on a given airfoil in nonlinear compressible flow.placebo 发表于 2025-3-29 11:55:14
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978-3-642-81007-7Springer-Verlag, Berlin/Heidelberg 1976DRILL 发表于 2025-3-30 07:44:14
Some Developments in Unsteady Transonic Flow Researchproblems. The study of unsteady flows helps one to achieve an improved understanding of steady flows, in particular as to the permanence and realizability of a particular steady flow and how typical transonic nonlinear effects develop in time. The engineering interest derives primarily from the prob