Toward a Practical Method for Hypersonic Transition Prediction Based on Stability Correlations-Reference-Cited by-同舟云学术

Toward a Practical Method for Hypersonic Transition Prediction Based on Stability Correlations

Published:2020-10 Issue:10 Volume:58 Page:4475-4484
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Paredes Pedro,Venkatachari Balaji,Choudhari Meelan M.,Li Fei,Chang Chau-Lyan,Zafar Muhammad I.,Xiao Heng

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J059407

Reference39 articles.

1. MackL. “Boundary Layer Linear Stability Theory (Special Course on Stability and Transition of Laminar Flow),” AGARD–R–709, Neuilly-Sur-Seine, France, 1984, pp. 3.1–3.81.

2. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies

3. Nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flow

4. Mach 10 Boundary Layer Transition Experiments on Sharp and Blunted Cones (Invited)

5. Nose-Tip Bluntness Effects on Transition at Hypersonic Speeds

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