Applied Hydro- and Aeromechanics: Based on Lectures of L. Prandtl, Band 2Courier Corporation, 01.01.1957 - 311 Seiten Prandtl was one of the great theorists of aerodynamics and this work has long been considered one of the finest introductory works in the field. Topics include flow through pipes, Prandtl's own work on boundary layers, drag, airfoil theory, and entry conditions for flow in a pipe. |
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airfoil anemometer angle of attack aspect ratio becomes Bernoulli's equation biplane Blasius bound vortex boundary layer calculated channel circular circulation constant critical Reynolds cross section curve cylinder decrease determined diameter direction distance drag coefficient eddy entrance equal equation experimental experiments flat plate flow round Flugtech fluid footnote formula friction drag function German Göttingen half body increase induced drag inertia forces infinite infinity Investigations Kármán kinetic energy laminar flow length lift distribution manometer means measured method momentum theorem motion Motorluftschiffahrt obtained particles plane potential flow Prandtl pressure distribution pressure drop pressure integral region result rotating seen shape shown in Fig shows skin friction span sphere starting vortex streamline picture surface theory tion tube turbulent flow various velocity distribution vortex band vortices wall wind tunnel wing zero ди ду дх