Numerical and Physical Aspects of Aerodynamic Flows II
Published on 3. October 2013
Book
Paperback/Softback
XI, 416 pages
978-3-662-09016-9 (ISBN)
Description
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.
More details
Edition
Softcover reprint of the original 1st ed. 1984
Language
English
Place of publication
Berlin
Germany
Publishing group
Springer Berlin
Target group
Professional and scholarly
Research
Illustrations
XI, 416 p.
Dimensions
Height: 235 mm
Width: 155 mm
Thickness: 24 mm
Weight
651 gr
ISBN-13
978-3-662-09016-9 (9783662090169)
DOI
10.1007/978-3-662-09014-5
Schweitzer Classification
Other editions
Additional editions
E-Book
06/2013
Springer
€96.29
Available for download
Book
12/1983
Springer
€85.59
Article exhausted; check different version
Content
General Review.- The Calculation of Two-Dimensional Flow Past Airfoils.- Keynote Paper.- Wing Design and Analysis-Your Job.- 1. Navier-Stokes Methods.- 1. Time-Dependent Finite-Difference Simulation of Unsteady Interactive Flows.- 2. Global Solution Procedures for Incompressible Laminar Flow with Strong Pressure Interaction and Separation.- 3. Measurements and Calculations of a Separating Boundary-Layer and the Downstream Wake.- 4. Numerical Simulation of Turbulent Trailing Edge Flows.- 5. Viscous-Inviscid Matching Using Imbedded Navier-Stokes Solutions.- 2. Interactive Methods and Measurements: Subsonic Flows.- 6. A Survey of Recent Work on Interacted Boundary-Layer Theory for Flow With Separation.- 7. Prediction of Subsonic Separation Bubbles on Airfoils by Viscous-Inviscid Interaction.- 8. A Calculation Method of Leading-Edge Separation Bubbles.- 9. An Interactive Approach to Subsonic Flows with Separation.- 10. Viscous/Inviscid Interaction Analysis of Asymmetric Trailing-Edge Flows.- 11. A Comparison Between the Predicted and Experimental Characteristics of a NACA 643-418 Aerofoil at Low Reynolds Numbers.- 12. Measurements of Attached and Separated Turbulent Flows in the Trailing-Edge Regions of Airfoils.- 3. Interactive Methods: Transonic Flows.- 13. Numerical Viscous-Inviscid Interaction in Steady and Unsteady Flows.- 14. Computation of Transonic Viscous-Inviscid Interacting Flow.- 15. Unsteady Viscous Transonic Flow Computations Using the LTRAN2-NLR Code Coupled with Green's Lag-Entrainment Method.- 16. On the Coupling of Boundary-Layer and Euler Equation Solutions.- 17. Investigation of Compressible Laminar, Boundary-Layer Solution Behavior at Separation Using a Displacement Thickness-Based Normal Scaling.- 18. Transonic Small Disturbance CalculationsIncluding Entropy Corrections.- 19. A Modified Shock-Point Operator with Stagnation-Density Correction.- 4. Analytical Methods.- 20. The Interaction Between a Steady Laminar Boundary-Layer and an Oscillating Flap: The Condensed Problem.- 21. Application of Unsteady Laminar Triple-Deck Theory to Viscous-Inviscid Interactions From an Oscillating Flap in Supersonic Flow.- 22. Interactive Separation From a Fixed Wall.- References.