Fully Local Formulation of a Transition Closure Model for Transitional Flow Simulations-Reference-Cited by-同舟云学术

Fully Local Formulation of a Transition Closure Model for Transitional Flow Simulations

Published:2016-10 Issue:10 Volume:54 Page:3015-3023
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Xu Jiakuan¹,Bai Junqiang¹,Qiao Lei¹,Zhang Yang¹,Fu Ziyuan¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, Shaanxi, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054808

Reference40 articles.

1. SmithA. M. O.GamberoniN. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Co., Rept. ES-26388, Long Beach, CA, 1956.

2. Van IngenJ. L. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Delft Univ. of Technology, Rept. VTH-74, Delft, The Netherlands, 1956.

3. MackL. M. “Transition Prediction and Linear Stability Theory,” AGARD CP-224, 1977, pp. 1–22.

4. BertolottiF. P. “Linear and Nonlinear Stability of Boundary Layers with Streamwise Varying Properties,” Ph.D. Thesis, Ohio State Univ., Columbus, OH, 1990.

5. Viscous-inviscid analysis of transonic and low Reynolds number airfoils

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