Nose-Tip Transition Control by Surface Roughness on a Hypersonic Sphere

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Journal of Flow Control, Measurement & Visualization

ISSN Print: 2329-3322
ISSN Online: 2329-3330
www.scirp.org/journal/jfcmv
E-mail: jfcmv@scirp.org

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"Nose-Tip Transition Control by Surface Roughness on a Hypersonic Sphere"
written by Kiran Joy Irimpan, Viren Menezes, K. Srinivasan, Hamid Hosseini,
published by Journal of Flow Control, Measurement & Visualization, Vol.6 No.3, 2018

has been cited by the following article(s):

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CrossRef

[1]	Surface roughness and model scale influences on forebody aerothermodynamics
	Aerospace Science and Technology, 2022

[2]	Stagnation heat flux estimation in spherically blunt axisymmetric hypersonic models
	Proceedings of the Institution of …, 2022

[3]	Calculation of Aerodynamic Characteristics of Hypersonic Vehicles Based on the Surface Element Method
	Advances in Aerospace Science and …, 2022

[4]	Hypersonic Incident Shock-Boundary Layer Interaction Control by Wavy Patches
	2020

[5]	粗糙元对高超声速边界层转捩影响的研究进展
	实验流体力学, 2018

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