Shock Control Bump Robustness Enhancement-Reference-Cited by-同舟云学术

Shock Control Bump Robustness Enhancement

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Nuebler Klemens¹,Lutz Thorsten¹,Kraemer Ewald¹,Colliss Simon²,Babinsky Holger²

Affiliation:

1. University of Stuttgart

2. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-46

Reference12 articles.

1. Drag Reduction by Shock and Boundary Layer Control

2. Two-equation eddy-viscosity turbulence models for engineering applications

3. An experimental investigation of three-dimensional shock control bumps applied to transonic airfoils

4. 5B. König: The Aerodynamic Potential of Shock Control Bumps on Transonic Transport Aircraft, PhD Thesis,Institute for Aerodynamics and Gas Dynamics, Universityof Stuttgart, to be published.

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