Modeling of Transonic Transitional Three-Dimensional Flows for Aerodynamic Applications-Reference-Cited by-同舟云学术

Modeling of Transonic Transitional Three-Dimensional Flows for Aerodynamic Applications

Published:2021-09 Issue:9 Volume:59 Page:3598-3610
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Boiko Andrey V.¹,Demyanko Kirill V.²,Kirilovskiy Stanislav V.¹,Nechepurenko Yuri M.²,Poplavskaya Tatiana V.¹

Affiliation:

1. Khristianovich Institute of Theoretical and Applied Mechanics, 630090, Novosibirsk, Russia

2. Marchuk Institute of Numerical Mathematics, 119333, Moscow, Russia

Funder

Russian Science Foundation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060174

Reference49 articles.

1. Engineering modeling of the laminar–turbulent transition: Achievements and problems (Review)

2. Physics of Transitional Shear Flows

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

4. SmithA. M. O.GamberoniN. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Company Rept. ES 26388, Santa Monica, CA, 1956.

5. MalikM. R. “COSAL: A Black-Box Compressible Stability Analysis Code for Transition Prediction in Three-Dimensional Boundary Layers,” NASA CR-65925, 1982.

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Ensuring of technological sovereignty of Russia in metallurgy and machine building;Вестник Российской академии наук;2024-08-15

2. Numerical Simulation of Swept-Wing Laminar–Turbulent Flow in the Presence of Two-Dimensional Surface Reliefs;Fluids;2024-04-19

3. USING TWO-PARAMETER VELOCITY PROFILES FOR THREE-DIMENSIONAL BOUNDARY LAYERS;Journal of Applied Mechanics and Technical Physics;2023-12

4. On the stability of supersonic boundary layer in interaction with weak shock waves;E3S Web of Conferences;2023

5. On predicting the onset of the transition to turbulence in the three-dimensional boundary layer on a swept wing;ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS;2023