Page 58 - 48Fundamentals of Compressible Fluid Mechanics
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20                                          CHAPTER 1. INTRODUCTION

                                            understanding, and many are still used today. Therefore many referred to him as
                                            the father of modern fluid mechanics. Ludwig Prandtl died in G¨ ottingen, Germany
                                            on August 15th 1953.
                                                     Prandtl’s other contributions include: the introduction of the Prandtl num-
                                            ber in fluid mechanics, airfoils and wing theory (including theories of aerodynamic
                                            interference, wing-fuselage, wing-propeller, biplane, etc); fundamental studies in
                                            the wind tunnel, high speed flow (correction formula for subsonic compressible
                                            flows), theory of turbulence. His name is linked to the following:

                                                • Prandtl number (heat transfer problems)

                                                • Prandtl-Glauert compressibility correction
                                                • Prandtl’s boundary layer equation

                                                • Prandtl’s lifting line theory
                                                • Prandtl’s law of friction for smooth pipes

                                                • Prandtl-Meyer expansion fans (supersonic flow)

                                                • Prandtl’s Mixing Length Concept (theory of turbulence)


                                            1.3.5.7  E.R.G. Eckert
                                            Eckert was born in 1904 in Prague,
                                            where he studied at the German Insti-
                                            tute of Technology. During World War
                                            II, he developed methods for jet engine
                                            turbine blade cooling at a research lab-
                                            oratory in Prague. He emigrated to the
                                            United States after the war, and served
                                            as a consultant to the U.S. Air Force
                                            and the National Advisory Committee
                                            for Aeronautics before coming to Min-
                                            nesota.
                                                     Eckert developed the under-  Fig. 1.12: The photo of Ernst Rudolf George
                                            standing of heat dissipation in relation to  Eckert with the author’s family
                                            kinetic energy, especially in compress-
                                            ible flow.  Hence, the dimensionless
                                            group has been designated as the Eckert number, which is associated with the
                                            Mach number. Schlichting suggested this dimensionless group in honor of Eckert.
                                            In addition to being named to the National Academy of Engineering in 1970, He
                                            authored more than 500 articles and received several medals for his contributions
                                            to science. His book ”Introduction to the Transfer of Heat and Mass,” published in
                                            1937, is still considered a fundamental text in the field.
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