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New Results in Numerical and Experimental Fluid Mechanics VIII

Contributions to the 17th STAB/DGLR Symposium Berlin, Germany 2010

  • Book
  • © 2013

Overview

Editors:
  1. Andreas Dillmann

    1. und Raumfahrt (DLR), Institut für Aerodynamik und, Deutsches Zentrum für Luft-, Göttingen, Germany

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  2. Gerd Heller

    1. Airbus Deutschland, Bremen, Germany

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  3. Hans-Peter Kreplin

    1. und Raumfahrt (DLR), Institut für Aerodynamik und, Deutsches Zentrum für Luft-, Göttingen, Germany

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  4. Wolfgang Nitsche

    1. , Institut für Luft- und Raumfahrt, TU Berlin, Berlin, Germany

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  5. Inken Peltzer

    1. Beechcraft Berlin aviation GmbH, Schönefeld, Germany

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  • Latest research in numerical and experimental fluid mechanics and aerodynamics for aerospace and other applications
  • Collection of contributions presented at the 17th Symposium of the STAB (German Aero-space Aerodynamics Association)
  • Addresses both academics and professionals working in the field of computational fluid dynamics
  • Edited and written by leading experts in the field

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 121)

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Table of contents (88 chapters)

  1. Front Matter

    Pages 1-15
    Download chapter PDF

  2. Investigation of the Impact of Simplifying the Aircraft Geometry on the Characteristics of the Vertical Tailplane

    • Anna Kröhnert, Lutz Gebhardt
    Pages 1-8

  3. Aerodynamic Optimization of a High-Lift System with Kinematic Constraints

    • Dirk M. Franke
    Pages 9-16

  4. Simulation of Store Separation Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations

    • N. Schade
    Pages 17-24

  5. Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet Configuration

    • Arno Ronzheimer, Martin Hepperle, Joël Brezillon, Olaf Brodersen, Jan Lieser
    Pages 25-32

  6. Analytical Design of an Inlet Distortion Generator and Its Experimental and Numerical Validation

    • Andreas Lesser, Sonja Schulze, Reinhard Niehuis, Christian Kähler, Jan Lieser
    Pages 33-41

  7. Wake Measurements to Assess the Flow-Structure Interaction of an Elasto-flexible Morphing Wing Configuration

    • B. Beguin, C. Breitsamter, N. Adams
    Pages 43-50

  8. Aerodynamic Characteristics of the Blended Wing Body ACFA2020

    • Michael Meyer, Christian Breitsamter
    Pages 51-58

  9. Development of the Adjoint Approach for Aeroelastic Wing Optimization

    • Mohammad Abu-Zurayk, Joël Brezillon
    Pages 59-66

  10. Application of a Coupling of Flight Mechanics and Aerodynamics to Predict the SHEFEX I Ascent Phase

    • J. Bartolomé Calvo, S. Wolkow, Th. Eggers
    Pages 67-74

  11. Experimental and Numerical Analysis of SHEFEX-II

    • Tarik Barth, Rolf Gehre, Thino Eggers, Jan Martinez Schramm, Alexander Wagner, Klaus Hannemann et al.
    Pages 75-83

  12. Investigation on Turbulence Structures in the Wake of a Generic Rocket Configuration

    • C. Christian Wolf, Rolf Henke, Ralf Hörnschemeyer
    Pages 85-92

  13. Thermal Fluid-Structure-Interaction on a Flat-Plate Model in Hypersonic High-Enthalpy Flow

    • M. Costantini, B. Esser, A. Gülhan
    Pages 93-100

  14. Numerical Generation of a Flush Air Data System for the Hypersonic Flight Experiment HIFiRE 7

    • C. Bode, Th. Eggers, M. Smart
    Pages 101-108

  15. Characterization of a Free-Molecular Pressure Probe Employing Gas-Kinetic Simulation

    • Martin Grabe, Georg Dettleff, Rolf-D. Boettcher, Klaus Hannemann
    Pages 109-116

  16. Wind Tunnel and Flight Tests with Active Flow Control on a S10 Glider Configuration

    • T. Grund, W. Nitsche
    Pages 117-124

  17. Evaluation of Passive and Active Secondary Flow Control in a High Speed Compressor Cascade with Different Measurement Techniques

    • Karsten Liesner, Robert Meyer
    Pages 125-133

  18. Parameter Study for a Slatless 2D High-Lift Airfoil with Active Separation Control Using a URANS Approach

    • V. Ciobaca
    Pages 135-142

  19. Influence of the Actuator Jet Angle on the Reattachment Process with Pulsed Excitation

    • M. Hecklau, D. Pieren Salazar, W. Nitsche
    Pages 143-150

  20. Optimal Control of a Plane Jet Using the Adjoint Method

    • Daniel Marinc, Holger Foysi
    Pages 151-159
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Keywords

About this book

This volume contains the contributions to the 17th Symposium of STAB (German Aerospace Aerodynamics Association). STAB includes German scientists and engineers from universities, research establishments and industry doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but also for other applications. Many of the contributions collected in this book present results from national and European Community sponsored projects. This volume gives a broad overview of the ongoing work in this field in Germany and spans a wide range of topics: airplane aerodynamics, multidisciplinary optimization and new configurations, hypersonic flows and aerothermodynamics, flow control (drag reduction and laminar flow control), rotorcraft aerodynamics, aeroelasticity and structural dynamics, numerical simulation, experimental simulation and test techniques, aeroacoustics as well as the new fields of biomedical flows, convective flows, aerodynamics and acoustics of high-speed trains.

Editors and Affiliations

  • und Raumfahrt (DLR), Institut für Aerodynamik und, Deutsches Zentrum für Luft-, Göttingen, Germany

    Andreas Dillmann, Hans-Peter Kreplin

  • Airbus Deutschland, Bremen, Germany

    Gerd Heller

  • , Institut für Luft- und Raumfahrt, TU Berlin, Berlin, Germany

    Wolfgang Nitsche

  • Beechcraft Berlin aviation GmbH, Schönefeld, Germany

    Inken Peltzer

Bibliographic Information

  • Book Title: New Results in Numerical and Experimental Fluid Mechanics VIII

  • Book Subtitle: Contributions to the 17th STAB/DGLR Symposium Berlin, Germany 2010

  • Editors: Andreas Dillmann, Gerd Heller, Hans-Peter Kreplin, Wolfgang Nitsche, Inken Peltzer

  • Series Title: Notes on Numerical Fluid Mechanics and Multidisciplinary Design

  • DOI: https://doi.org/10.1007/978-3-642-35680-3

  • Publisher: Springer Berlin, Heidelberg

  • eBook Packages: Engineering, Engineering (R0)

  • Copyright Information: Springer-Verlag Berlin Heidelberg 2013

  • Hardcover ISBN: 978-3-642-35679-7Published: 27 December 2012

  • Softcover ISBN: 978-3-642-43192-0Published: 29 January 2015

  • eBook ISBN: 978-3-642-35680-3Published: 27 December 2012

  • Series ISSN: 1612-2909

  • Series E-ISSN: 1860-0824

  • Edition Number: 1

  • Number of Pages: XVIII, 750

  • Topics: Aerospace Technology and Astronautics, Fluid- and Aerodynamics, Engineering Fluid Dynamics

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