Transition prediction in infinite swept wings using Navier–Stokes computations and linear stability theory-Reference-Cited by-同舟云学术

Transition prediction in infinite swept wings using Navier–Stokes computations and linear stability theory

Published:2004-07 Issue:17-19 Volume:82 Page:1551-1560
ISSN:0045-7949
Container-title:Computers & Structures
language:en
Short-container-title:Computers & Structures

Author:

Sousa J.M.M.,Silva L.M.G.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,General Materials Science,Modeling and Simulation,Civil and Structural Engineering

Reference26 articles.

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2. Van Ingen JL. A suggested semi-empirical method for the calculation of the boundary layer transition region. Report VTH-74, University of Delft, The Netherlands, 1956

3. Arnal D. Boundary layer transition: predictions based on linear theory. AGARD Report No. 793. Special course on progress in transition modelling, 1994

4. Aircraft laminar flow control;Joslin;Ann. Rev. Fluid Mech.,1998

5. Transition prediction in external flows via linear stability theory;Bushnell,1988

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