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Grenzschicht-Theorie (German, Hardcover, 10., uberarb. Aufl. 2006): E. Krause Grenzschicht-Theorie (German, Hardcover, 10., uberarb. Aufl. 2006)
E. Krause; H. Schlichting; Assisted by H. Jr. Oertel; Klaus Gersten
R8,318 Discovery Miles 83 180 Ships in 10 - 15 working days

Die Uberarbeitung fur die 10. deutschsprachige Auflage von Hermann Schlichtings Standardwerk wurde wiederum von Klaus Gersten geleitet, der schon die umfassende Neuformulierung der 9. Auflage vorgenommen hatte. Es wurden durchgangig Aktualisierungen vorgenommen, aber auch das Kapitel 15 von Herbert Oertel jr. neu bearbeitet. Das Buch gibt einen umfassenden Uberblick uber den Einsatz der Grenzschicht-Theorie in allen Bereichen der Stromungsmechanik. Dabei liegt der Schwerpunkt bei den Umstromungen von Korpern (z.B. Flugzeugaerodynamik).

Das Buch wird wieder den Studenten der Stromungsmechanik wie auch Industrie-Ingenieuren ein unverzichtbarer Partner unerschopflicher Informationen sein."

An Approximate Method for Calculation of the Laminar Boundary Layer with Suction for Bodies of Arbitrary Shape (Paperback): H.... An Approximate Method for Calculation of the Laminar Boundary Layer with Suction for Bodies of Arbitrary Shape (Paperback)
H. Schlichting
R509 Discovery Miles 5 090 Ships in 10 - 15 working days

Various ways were tried recently to decrease the friction drag of a body in a flow; they all employ influencing the boundary layer. One of them consists in keeping the boundary layer Laminar by suction; promising tests have been carried out. Since for large Reynolds numbers the friction drag of the laminar boundary layer is much lower than that of the turbulent boundary layer, a considerable saving in drag results from keeping the boundary layer laminar, even with the blower power required for suction taken into account. The boundary layer is kept laminar by suction in two ways: first, by reduction of the thickness of the boundary layer and second, by the fact that the suction changes the form of the velocity distribution so that it becomes more stable, in a manner similar to the change by a pressure drop. There by the critical Reynolds number of the boundary layer (USigma*/V) (sub crit) becomes considerably higher than for the case without suction. This latter circumstance takes full effect only if continuous suction is applied which one might visualize realized through a porous wall. Thus the suction quantities required for keeping the boundary layer laminar become so small that the suction must be regarded as a very promising auxiliary means for drag reduction.

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