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Fluid dynamics / Boundary layer / Tollmien–Schlichting wave / Airfoil / Laminar flow / Lift / Reynolds number / Navier–Stokes equations / Swept wing / Aerodynamics / Aerospace engineering / Fluid mechanics


Preliminary Investigation Into the Effects of Cross-Flow on Low Reynolds Number Transition
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Document Date: 2011-09-07 13:54:26


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File Size: 3,14 MB

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City

Honolulu / Cambridge / /

Company

Astronautics Inc. / /

Country

United States / /

/

Facility

U.S.A. Per-Olof Persson† University of California Berkeley / American Institute of Aeronautics / Jaime Peraire§ Massachusetts Institute of Technology / Low Reynolds Number Transition Alejandra Uranga∗ Massachusetts Institute of Technology / /

IndustryTerm

gas equation / computing / post-processing tasks / time-dependent systems / internal energy / energy / /

Organization

U.S.A. Per-Olof Persson† University / Department of Mathematics / University of California / Massachusetts Institute of Technology / American Institute of Aeronautics / /

Person

Jaime Peraire / /

/

Position

author / Assistant Professor / Professor of Fluid Dynamics / Professor / /

Product

swept wing / /

ProvinceOrState

California / Massachusetts / /

Technology

Fluid Dynamics / simulation / /

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