Effect of compressibility on plasma-based transition control for a wing with leading-edge excrescence-Reference-Cited by-同舟云学术

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Effect of compressibility on plasma-based transition control for a wing with leading-edge excrescence

Published:2017-03-16 Issue:3 Volume:31 Page:156-173
ISSN:1061-8562
Container-title:International Journal of Computational Fluid Dynamics
language:en
Short-container-title:International Journal of Computational Fluid Dynamics

Author:

Rizzetta D. P.¹,Visbal M. R.¹

Affiliation:

1. Air Force Research Laboratory, Wright-Patterson Air Force Base, Dayton, OH, USA

Funder

U.S. Air Force Office of Scientific Research

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/10618562.2017.1316490

Reference51 articles.

1. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations

2. An Approach to Measuring Step Excrescence Effects in the Presence of a Pressure Gradient

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