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Flow characteristics of various three-dimensional rounded contour bumps in a Mach 1.3 freestream

  • Published:2017-01 Issue: Volume:80 Page:228-243
  • ISSN:0894-1777
  • Container-title:Experimental Thermal and Fluid Science
  • language:en
  • Short-container-title:Experimental Thermal and Fluid Science

Author:

Lo Kin Hing,Kontis Konstantinos

Funder

Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference44 articles.

1. Toward designing with three-dimensional bumps for lift/drag improvement and buffet alleviation;Eastwood;AIAA J.,2012

2. Shock control bumps on flexible and trimmed transport aircraft in Transonic Flow;König,2007

3. Numerical and experimental validation of three-dimensional shock control bumps;König;J. Aircraft,2009

4. Three-dimensional contour bumps for transonic wing drag reduction;Qin;Proc. IMech E Part G J. Aerosp. Eng.,2008

5. A combined experimental and numerical study of flow structures over three-dimensional shock control bumps;Wong;J. Aerosp. Sci. Technol.,2008

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