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Published in 2019 at "International Journal of Heat and Mass Transfer"
DOI: 10.1016/j.ijheatmasstransfer.2019.03.012
Abstract: Abstract Due to the lacking of knowledge and incomplete information about the closure coefficients in Menter Shear Stress Transport (SST) turbulence model, numerical predictions of hypersonic flow heat transfer possess some uncertainties. The objective of…
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Keywords:
hypersonic flow;
heat;
uncertainty;
model ... See more keywords
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Published in 2021 at "Physics of Fluids"
DOI: 10.1063/5.0040514
Abstract: This study investigates the origin and sustenance of self-induced oscillations of shock structures in a hypersonic flow over a double wedge configuration. Previously, various researchers have considered the double wedge flow configuration for inviscid flow…
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Keywords:
flow double;
hypersonic flow;
geometry;
wedge ... See more keywords
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Published in 2018 at "SIMULATION"
DOI: 10.1177/0037549717733051
Abstract: The present work provides a detailed comparative study of the hypersonic flow past spherically blunted and parabolic nose cones at a Mach number of 5.8, numerically. The main focus of the paper is to determine…
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Keywords:
hypersonic flow;
comparative study;
drag;
parabolic nose ... See more keywords
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Published in 2025 at "Optics express"
DOI: 10.1364/oe.567227
Abstract: This article presents the first demonstration of the tunable 5th harmonic of a Nd:YAG pulse-burst laser used for single-shot velocity and acceleration measurements via Nitric-oxide ionization induced Flow Tagging and Imaging. This demonstration was performed…
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Keywords:
hypersonic flow;
5th harmonic;
ionization;
nitric oxide ... See more keywords
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Published in 2018 at "Scientia Iranica"
DOI: 10.24200/sci.2018.20339
Abstract: Use of spike on a hemispherical body changes the flow field and hence the aerodynamic drag. Computational studies have been made to obtain the flow field around a hemispherical body with spikes at a hypersonic…
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Keywords:
length;
hypersonic flow;
spikes hypersonic;
spike ... See more keywords
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Published in 2025 at "Journal of Spacecraft and Rockets"
DOI: 10.2514/1.a36312
Abstract: Hypersonic flow over axisymmetric bodies with four evenly spaced fins was investigated computationally. The test conditions encompassed a freestream Mach number of 5.9 and Reynolds numbers based on body length of [Formula: see text] and…
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Keywords:
wave boundary;
shock wave;
boundary layer;
hypersonic flow ... See more keywords