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Numerical and Phyical Aspects of Aerodynamic Flow III

  • Conference proceedings
  • © 1986

Overview

Editors:
  1. Tuncer Cebeci

    1. Douglas Aircraft Company, Long Beach, USA
      California State University, Long Beach, USA

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Table of contents (25 papers)

  1. Front Matter

    Pages i-ix
    Download chapter PDF

  2. Calculation Methods for Aerodynamic Flows—A Review

    1. Calculation Methods for Aerodynamic Flows—a Review

      • Tuncer Cebeci, J. H. Whitelaw
      Pages 1-19

  3. Stability and Transition

    1. Front Matter

      Pages 21-21
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    2. Stewartson Memorial Lecture: Hydrodynamic Stability and Turbulent Transition

      • J. T. Stuart
      Pages 23-38

    3. Transition Calculations in Three-Dimensional Flows

      • R. Michel, E. Coustols, D. Arnal
      Pages 39-56

    4. Transitional Spot Formation Rate in Two-Dimensional Boundary Layers

      • R. Narasimha, J. Dey
      Pages 57-74

  4. Two-Dimensional Flows

    1. Front Matter

      Pages 75-75
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    2. The Computation of Viscid-Inviscid Interaction on Airfoils with Separated Flow

      • R. E. Melnik, J. W. Brook
      Pages 77-101

    3. Laminar Separation Studied as an Airfoil Problem

      • H. K. Cheng, C. J. Lee
      Pages 102-125

    4. A Quasi-simultaneous Finite Difference Approach for Strongly Interacting Flow

      • David E. Edwards, James E. Carter
      Pages 126-142

    5. Newton Solution of Coupled Euler and Boundary-Layer Equations

      • M. Drela, M. Giles, W. T. Thompkins Jr.
      Pages 143-154

    6. Aerofoils at Low Reynolds Numbers—Prediction and Experiment

      • P. M. Render, J. L. Stollery, B. R. Williams
      Pages 155-167

    7. Comparison of Interactive and Navier—Stokes Calculations of Separating Boundary-Layer Flows

      • D. Adair, B. E. Thompson, J. H. Whitelaw, B. R. Williams
      Pages 168-183

    8. Significance of the Thin-Layer Navier—Stokes Approximation

      • F. G. Blottner
      Pages 184-197

    9. A Comparison of Interactive Boundary-Layer and Thin-Layer Navier—Stokes Procedures

      • Unmeel Mehta, K. C. Chang, Tuncer Cebeci
      Pages 198-215

    10. Development of a Navier—Stokes Analysis to Investigate the Mechanism of Shock-Wave—Boundary-Layer Interactions

      • D. V. Roscoe, H. J. Gibeling, H. McDonald, S. J. Shamroth
      Pages 216-231
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Keywords

About this book

The Third Symposium on Numerical and Physical Aspects of Aerodynamic Flows, like its immediate predecessor, was organized with emphasis on the calculation of flows relevant to aircraft, ships, and missiles. Fifty-five papers and 20 brief communications were presented at the Symposium, which was held at the California State University at Long Beach from 21 to 24 January 1985. A panel discussion was chaired by A. M. O. Smith and includeq state­ ments by T. T. Huang, C. E. lobe, l. Nielsen, and C. K. Forester on priorities for future research. The first lecture in memory of Professor Keith Stewartson was delivered by J. T. Stuart and is reproduced in this volume together with a selection of the papers presented at the Symposium. In Volume II of this series, papers were selected so as to provide a clear indication of the range of procedures available to represent two-dimensional flows, their physical foundation, and their predictive ability. In this volume, the emphasis is on three-dimensional flows with a section of five papers concerned with unsteady flows and a section of seven papers on three­ dimensional flows: The papers deal mainly with calculation methods and encompass subsonic and transonic, attached and separated flows. The selec­ tion has been made so as to fulfill the same purpose for three-dimensional flows as did Volume II for two-dimensional flows.

Editors and Affiliations

  • Douglas Aircraft Company, Long Beach, USA

    Tuncer Cebeci

  • California State University, Long Beach, USA

    Tuncer Cebeci

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