k-e Model for Predicting Transitional Boundary-Layer Flows Under Zero-Pressure Gradient
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Taejon 305-701, Republic of Korea
2. Hoseo University, Asan, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1527
Reference23 articles.
1. The 1991 IGTI Scholar Lecture: The Role of Laminar-Turbulent Transition in Gas Turbine Engines
2. 2Cebeci, T., and Smith, A. M. O., Analysis of Turbulent Boundary Layers, Academic Press, New York, 1974, pp.234-239.
3. One-Equation Near-Wall Turbulence Modeling With the Aid of Direct Simulation Data
4. Application of the energy-dissipation model of turbulence to the calculation of flow near a spinning disc
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