Effects of temperature on drag reduction in a subsonic turbulent boundary layer via micro-blowing array
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference39 articles.
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3. Review of research into the concept of the microblowing technique for turbulent skin friction reduction;Hwang;Prog Aerosp Sci,2004
4. Experimental study of characteristics of micro-hole porous skins for turbulent skin friction reduction;Hwang,2002
5. Tillman T, Hwang D. Drag reduction on a large-scale nacelle using a micro-blowing technique. Reston: AIAA; 1999. Report No.:AIAA-1999-0130.
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