High-Fidelity Simulations of Discrete Roughness Boundary-Layer Transition with Added Perturbations-Reference-Cited by-同舟云学术

High-Fidelity Simulations of Discrete Roughness Boundary-Layer Transition with Added Perturbations

Published:2020-09 Issue:5 Volume:57 Page:1079-1091
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Tufts Matthew W.¹,Bisek Nicholas J.¹,Kimmel Roger L.¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7542

Funder

Air Force Research Laboratory

Air Force Office of Scientific Research under Dr. Ivett Leyva

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.A34737

Reference28 articles.

1. Hypersonic and High-Temperature Gas Dynamics, Second Edition

2. PSE Analysis of Crossflow Instability on HIFiRE 5b Flight Test

3. Van IngenJ. L. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Dept. of Aerospace Engineering, Delft Univ. of Technology, Report V.T.H. 74, Delft, The Netherlands, 1956.

4. ReedH. L.ReshotkoE.SaricW. S. “Receptivity: The Inspiration of Mark Morkovin,” AIAA Paper 2015-2471, 2015. 10.2514/6.2015-2471

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