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  • Conference proceedings
  • © 1984

Numerical and Physical Aspects of Aerodynamic Flows II

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Table of contents (24 papers)

  1. Front Matter

    Pages i-xi
  2. Calculation of Two-Dimensional Flow Past Airfoils

    1. Calculation of Two-Dimensional Flow Past Airfoils

      • T. Cebeci, K. Stewartson, J. H. Whitelaw
      Pages 1-40
  3. Wing Design and Analysis—Your Job

    1. Wing Design and Analysis—Your Job

      • A. M. O. Smith
      Pages 41-59
  4. Navier-Stokes Methods

    1. Front Matter

      Pages 61-61
    2. Time-Dependent Finite-Difference Simulation of Unsteady Interactive Flows

      • George S. Deiwert, Harry E. Bailey
      Pages 63-78
    3. Measurements and Calculations of a Separating Boundary-Layer and the Downstream Wake

      • D. Adair, B. E. Thompson, J. H. Whitelaw
      Pages 97-112
    4. Viscous-Inviscid Matching Using Imbedded Navier-Stokes Solutions

      • P. Bradshaw, M. A. Kavanagh, D. Mobbs
      Pages 125-138
  5. Interactive Methods: Transonic Flows

    1. Front Matter

      Pages 257-257
    2. Computation of Transonic Viscous-Inviscid Interacting Flow

      • D. L. Whitfield, J. L. Thomas, A. Jameson, W. Schmidt
      Pages 285-295

About this book

The Second Symposium on Numerical and Physical Aspects of Aerodynamic Flows was held at California State University, Long Beach, from 17 to 20 January 1983. Forty-eight papers were presented, including Keynote Lec­ tures by A. M. 0. Smith and J. N. Nielsen, in ten technical sessions which were supplemented and complemented by two Open Forum Sessions, involving a further sixteen technical presentations and a Panel Discussion on the "Identification of priorities for the development of calculation methods for aerodynamic bodies. " The Symposium was attended by 120 research workers from nine countries and, as in the First Symposium, provided a basis for research workers to communicate, to assess the present status of the subject and to formulate priorities for the future. In contrast to the First Symposium, the papers and discussion were focused more clearly on the subject of flows involving the interaction between viscous and inviscid regions and the calculation of pressure, velocity and temperature characteristics as a function of geometry, angle of attack and Mach number. Rather more than half the papers were concerned with two-dimensional configurations and the remainder with wings, missiles and ships. This volume presents a selection of the papers concerned with two­ dimensional flows and a review article specially prepared to provide essen­ tial background information and link the topics of the individual papers.

Editors and Affiliations

  • Douglas Aircraft Company, Long Beach, USA

    Tuncer Cebeci

  • California State University, Long Beach, USA

    Tuncer Cebeci

Bibliographic Information

Buy it now

Buying options

eBook USD 84.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book USD 109.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Other ways to access