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Titlebook: Aerodynamic Theory; A General Review of William Frederick Durand Book 1935 Berlin · Julius Springer 1935 Entwicklung.Entwurf.Pitch.Promoti

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期刊全称Aerodynamic Theory
期刊简称A General Review of
影响因子2023William Frederick Durand
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图书封面Titlebook: Aerodynamic Theory; A General Review of  William Frederick Durand Book 1935 Berlin · Julius Springer 1935 Entwicklung.Entwurf.Pitch.Promoti
影响因子Dieser Buchtitel ist Teil des Digitalisierungsprojekts Springer Book Archives mit Publikationen, die seit den Anfängen des Verlags von 1842 erschienen sind. Der Verlag stellt mit diesem Archiv Quellen für die historische wie auch die disziplingeschichtliche Forschung zur Verfügung, die jeweils im historischen Kontext betrachtet werden müssen. Dieser Titel erschien in der Zeit vor 1945 und wird daher in seiner zeittypischen politisch-ideologischen Ausrichtung vom Verlag nicht beworben.
Pindex Book 1935
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978-3-642-89628-6Berlin · Julius Springer 1935
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Organisationale Verortung des Controllings air, of producing a supporting or lifting force. This property has long been known and the most remarkable feature connected with it is that the lifting force may be very great compared with the resistance which the plane experiences in the direction opposite to its motion. The ratio of the support
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Allgemeiner Managementkreislaufs fluid. As already pointed out in the last section, this is the only case in which the fundamental problem of wing theory, . the calculation of velocity and pressure distribution around the moving airfoil, can be attacked in a direct way. The reason is that in the two-dimensional case, the motion a
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Organisationale Verortung des Controllings starting point the investigation of the influence of external forces upon the motion of a fluid. The basis for our deductions consequently will be formed by the equations of hydrodynamics completed with terms representing these external forces (see Division B I). The influence of viscosity will be
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https://doi.org/10.1007/978-3-322-92938-9bution of the velocity and of the vorticity in the wake has been calculated to the first order of small quantities only. The values of the velocity components ...... and of the components of the vorticity ...... are then given respectively by III (9.1) in conjunction with III (9.4), III (9.8) and by
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