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    4. Klassisk mekanik

    Numerical and Physical Aspects of Aerodynamic Flows IV

    AvTuncer Cebeci

    Häftad, Engelska, 2013

    1 086 kr

    Beställningsvara. Skickas inom 10-15 vardagar. Fri frakt över 249 kr.

    Beskrivning

    This volume contains a selection of the papers presented at the Fourth Symposium on Numerical and Physical Aspects of Aerodynamic Flows, which was held at the California State University, Long Beach, from 16-19 January 1989. It includes the Stewartson Memorial Lecture of Professor J. H. Whitelaw, and is divided into three parts. The first is a collection of papers that describe the status of current technology in two- and three-dimensional steady flows, the second deals with two- and three-dimensional unsteady flows, and the papers in the third address stability and transition. Each of the three parts begins with an overview of current research, as described in the following chapters. The individual papers are edited versions of the selected papers originally submitted to the symposium. Four years have passed since the Third Symposium, and certain trends be­ come clear if one compares the papers contained in this volume with those of previous volumes. There are more three- than two-dimensional problems consid­ ered in Part 1 and the latter address more difficult problems than in the past, for example, the extension to higher angles of attack, to transonic flow, to leading­ edge ice accretion, and to thick hydrofoils. The large number of papers in the first part reflects the emphasis of current research and development and the needs of industry.

    Produktinformation

    • Utgivningsdatum:2013-10-03
    • Mått:155 x 235 x 24 mm
    • Vikt:651 g
    • Format:Häftad
    • Språk:Engelska
    • Antal sidor:417
    • Förlag:Springer-Verlag Berlin and Heidelberg GmbH & Co. KG
    • ISBN:9783662026458

    Utforska kategorier

    • Klassisk mekanik inom Naturvetenskap och teknik
    • Matematisk fysik inom Naturvetenskap och teknik

    Innehållsförteckning

    • Stewartson Memorial Lecture: Experiments are Telling You Something.- 1. Two- and Three-Dimensional Steady Flows.- 1. Predictions of Airfoil Aerodynamic Performance Degradation Due to Icing.- 2. VISTRAFS: A Simulation Method for Strongly Interacting Viscous Transonic Flow.- 3. Coupling Procedures for Viscous-Inviscid Interaction for Attached and Separated Flows on Swept and Tapered Wings.- 4. New Possibilities of Viscous-Inviscid Numerical Techniques for Solving Viscous Flow Equations with Massive Separation.- 5. Prediction of Post-Stall Flows on Airfoils.- 6. Turbulence Characteristics of Trailing-Edge Flows on Thick and Thin Hydrofoils.- 7. Computational Fluid Dynamics at NASA Ames Research Center.- 8. 3-D Composite Velocity Solutions for Subsonic/Transonic Flows.- 9. Calculation of Transonic Flows for Novel Engine-Airframe Installations.- 10. Calculation of Three-Dimensional Boundary Layers Including Hypersonic Flows.- 11. Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurations.- 12. Numerical Simulation of Separated and Vortical Flows on Bodies at Large Angles of Attack.- 2. Two- and Three-Dimensional Unsteady Flows.- 13. The Relevance of Unsteady Aerodynamics for Highly Maneuverable and Agile Aircraft.- 14. Experimental and Computational Studies of Dynamic Stall.- 15. A Critique of the Experimental Aerodynamic Data Base for an Oscillating Straked Wing at High Angles.- 16. On the Effects of Wind Tunnel Turbulence on Steady and Unsteady Airfoil Characteristics.- 3. Stability and Transition.- 17. Applications and Suggested Directions of Transition Research.- 18. Prediction of Transition on Airfoils with Separation Bubbles, Swept Wings, and Bodies of Revolution at Incidence.- 19. Transition in Hypersonic Boundary Layers.- 20. Transition Phenomena on Airfoils Operating at Low Chord Reynolds Numbers in Steady and Unsteady Flow.- 21. Disturbance Growth in an Unstable Three-Dimensional Boundary Layer.- 22. Experiments in Swept-Wing Transition.- 23. Experimental Transition and Boundary-Layer Stability Analysis for a Slotted Swept Laminar Flow Control Airfoil.- 24. Leading-Edge Contamination and Relaminarization on a Swept Wing at Incidence.- References.- Index of Contributors.