Investigation on transition correlation of conical boundary layer in hypersonic wind tunnel experiments-Reference-Cited by-同舟云学术

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Investigation on transition correlation of conical boundary layer in hypersonic wind tunnel experiments

Published:2022-12 Issue: Volume:201 Page:329-339
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Lee Shibo,Duan Maochang,Tu Guohua,Wan Bingbing^ORCID,Chen Jianqiang,Yuan Xianxu

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Experimental study of several on aerodynamic problems on hypersonic vehicles;Li;Modern Defence Technology,2014

2. Hypersonic and High Temperature Gas Dynamics;Anderson,2006

3. Recent progress on hypersonic boundary-layer transition;Chen;Sci. Sin-Phys. Mech. Astron.,2019

4. Shock tunnel investigation of boundary-layer transition at M equals 5.5;Rushton;AIAA J.,2012

5. Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: the role of quiet tunnels;Schneider;Prog. Aero. Sci.,2015

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1. Enhancements to Linear Stability Solver-Based CFD-integrated Transition Prediction for High-Speed Flows;AIAA SCITECH 2024 Forum;2024-01-04

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