Numerical Study on the Ability of Shock Control Bumps for Buffet Control-Reference-Cited by-同舟云学术

Numerical Study on the Ability of Shock Control Bumps for Buffet Control

Published:2018-05 Issue:5 Volume:56 Page:1978-1987
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Mayer R.¹,Lutz T.¹,Krämer E.¹

Affiliation:

1. Institute of Aerodynamics and Gas Dynamics, University of Stuttgart, 70569 Stuttgart, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056737

Reference26 articles.

1. AshillP. R.FulkerJ. L.ShiresA. “A Novel Technique for Controlling Shock Strength of Laminar-Flow Aerofoil Sections,” DGLR Bericht Rept. 92-01-022, 1992, pp. 175–183.

2. Shock control on a swept wing

3. Three-dimensional shock control bumps: effects of geometry

4. Shock / Boundary Layer Interaction Control Using 3D Devices

5. Numerical and Experimental Validation of Three-Dimensional Shock Control Bumps

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