Drag Reduction by Shock and Boundary Layer Control Results of the Project EUROSHOCK II. Supported by the European Union 1996–1999

Drag Reduction by Shock and Boundary Layer Control Results of the Project EUROSHOCK II. Supported by the European Union 1996–1999 / edited by Egon Stanewsky, J. Delery, John Fulker, Paolo de Matteis.

This volume contains a thorough description of the EU-supported project EUROSHOCK II concerned with the investigation of active shock and boundary layer control to improve aircraft performance. Discussed are basic experiments, supplemented by Navier-Stokes computations, to improve and validate physi...

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Bibliographic Details
Corporate Author: SpringerLink (Online service)
Other Authors: Stanewsky, Egon (Editor), Delery, J. (Editor), Fulker, John (Editor), Matteis, Paolo de (Editor)
Format: eBook
Language:English
Published: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer, 2002.
Edition:1st ed. 2002.
Series:Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 80
Springer eBook Collection.
Subjects:
Fluid mechanics.
Mechanical engineering.
Computational intelligence.
Mechanics.
Mechanics, Applied.
Automotive engineering.
Vibration.
Dynamical systems.
Dynamics.
Electronic resources (E-books)
Online Access:Click to view e-book
Holy Cross Note:Loaded electronically.
Electronic access restricted to members of the Holy Cross Community.
Table of Contents:
  • Introduction
  • The EUROSHOCK II Project
  • Modeling of Active Control Phenomena
  • Numerical Simulation of Airfoil and Wing Flow with Control
  • Airfoil and Sheared-Wing Experiments with and Without Control
  • Benefits of Control Application to Aircraft Wings/Aircraft
  • Assessment of Shock and Boundary Layer Control - A Summary
  • Overall Conclusions and Future Work
  • Introduction to the Individual Contributions
  • Study of Control Devices Applied to a Transonic Shock Wave/Boundary Layer Interaction
  • Hybrid and Active Control of Shock Wave - Turbulent Boundary Layer Interaction and Perforated Plate Transpiration Flow
  • Active Control of Swept Shock Wave/Boundary Layer Interactions
  • Numerical Investigation of Active Shock Wave and Boundary Layer Control on Airfoils and Sheared Wings
  • Boundary Layer Coupling to Predict Steady and Unsteady Transonic Flows Past an Airfoil with and Without Shock Control
  • 2D Numerical Investigations of Shock and Boundary Layer Control Techniques.

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