Adapting Three-Dimensional Shock Control Bumps for Swept Flows-Reference-Cited by-同舟云学术

Adapting Three-Dimensional Shock Control Bumps for Swept Flows

Published:2017-03 Issue:3 Volume:55 Page:861-873
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Jones Natasha R.¹,Eastwood Jeremy P.¹,Jarrett Jerome P.¹

Affiliation:

1. University of Cambridge, Cambridge, England CB2 1PZ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J055169

Reference31 articles.

1. AshillP. R.FulkerJ. L.ShiresA. “A Novel Technique for Controlling Shock Strength of Laminar-Flow Aerofoil Sections,” DGLR Bericht 92-01, 1992, pp. 175–183, http://d-nb.info/931164648/04.

2. Toward Designing with Three-Dimensional Bumps for Lift/Drag Improvement and Buffet Alleviation

3. Synopsis of the Project EUROSHOCK II

4. Investigations on Shock Control Bumps for Infinite Swept Wings

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

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