Morphing Continuum Simulation of Transonic Flow over Axisymmetric Hill-Reference-Cited by-同舟云学术

Morphing Continuum Simulation of Transonic Flow over Axisymmetric Hill

Published:2018-11 Issue:11 Volume:56 Page:4321-4330
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wonnell Louis B.¹,Cheikh Mohamad I.¹,Chen James²

Affiliation:

1. Kansas State University, Manhattan, Kansas 66506

2. University at Buffalo, State University of New York, Buffalo, New York 14260

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057064

Reference39 articles.

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2. Comparison of LES and RANS calculations of the flow around bluff bodies

3. Implementation of k-w Turbulence Models in an Implicit Multigrid Method

4. LARGE-EDDY SIMULATION OF TURBULENT COMBUSTION

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

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