Roughness receptivity in swept-wing boundary layers – computations

International Journal of Engineering Systems Modelling and Simulation

Volumn 2, Issue 1-2, 2010, Pages 139-148

  Rhodes, Richard G ^a   Reed, Helen L ^a   Saric, William S ^a   Carpenter, Andrew L ^a   Neale, Tyler P ^a  

^a Department of Electrical and Computer Engineering   (United States)

Author keywords

3D boundary layers; computations; laminar flow control; receptivity; roughness; swept wings

Indexed keywords

EID: 78649502425     PISSN: 17559758     EISSN: 17559766     Source Type: Journal    
DOI: 10.1504/IJESMS.2010.031878     Document Type: Article

References (36)

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35. Recently relocated to the Department of Aerospace Engineering at Texas A&M University, http://aerospace-labs.tamu.edu.
36. The Braslow criteria suggest that the flow will not trip for roughness Reynolds number below 150 (von Doenhoff and Braslow, 1961).