Piotr doerffer u a (5 Ergebnisse)

Taschenbuch. Zustand: Neu. Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications | Pawel Flaszynski (u. a.) | Taschenbuch | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | x | Englisch | 2026 | Springer | EAN 9783031866074 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.…

Taschenbuch. Zustand: Neu. Transition Location Effect on Shock Wave Boundary Layer Interaction | Experimental and Numerical Findings from the TFAST Project | Piotr Doerffer (u. a.) | Taschenbuch | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | viii | Englisch | 2021 | Springer | EAN 9783030474638 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.…

Taschenbuch. Zustand: Neu. Progress in Hybrid RANS-LES Modelling | Papers Contributed to the 3rd Symposium on Hybrid RANS-LES Methods, Gdansk, Poland, June 2009 | Shia-Hui Peng (u. a.) | Taschenbuch | xii | Englisch | 2016 | Springer | EAN 9783662506615 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.…

Taschenbuch. Zustand: Neu. Recent Progress in Flow Control for Practical Flows | Results of the STADYWICO and IMESCON Projects | Piotr Doerffer (u. a.) | Taschenbuch | xi | Englisch | 2018 | Springer | EAN 9783319844305 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu. …

Hardcover. Zustand: New. HardCover. Pub Date: 2022-10-01 Pages: 288 Language: Chinese Publisher: Science Press Unsteady Effects of Shock-Induced Separation focuses on three basic configurations of transonic airfoil. nozzle flow. and oblique shock wave reflection Introduce the research progress of the unsteady problem of shock wave/boundary layer interference. give a large number of unsteady pressure and aerodynamic experimental data. and compare with the results of different numerical simulation methods. and evaluate.…