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Published in 2017 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2016.10.027
Abstract: Abstract An unsteady viscous numerical simulation is performed to study the starting process of a hypersonic nozzle coupled with a simplified inlet model in a shock tunnel under the condition of inflow Mach number higher…
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Keywords:
inlet;
shock tunnel;
hypersonic nozzle;
initial backpressure ... See more keywords
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Published in 2018 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2017.11.001
Abstract: Abstract Of all the possible outcomes of the shock interaction problem, Edney Type-III and Type-IV are considered to be of great importance as they lead to high heat transfer rates on the surface in the…
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Keywords:
shock tunnel;
type iii;
shock;
interaction ... See more keywords
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Published in 2018 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2017.12.013
Abstract: Abstract A shock tunnel is a representative type of ground-based equipment in the hypersonic field, which has the advantage of free stream of excellent quality. Accurate measurements of aerodynamic forces in the shock tunnel are…
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Keywords:
drag history;
shock tunnel;
shock;
start process ... See more keywords
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Published in 2017 at "Journal of Spacecraft and Rockets"
DOI: 10.2514/1.a33820
Abstract: Experiments to measure the forces and moments acting on a blunted-cone capsule model are conducted in the High Enthalpy Shock Tunnel Gottingen. A free-flying arrangement is employed, whereby the mo...
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Keywords:
shock tunnel;
capsule;
force moment;
free flying ... See more keywords
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Published in 2021 at "AIAA Journal"
DOI: 10.2514/1.j060596
Abstract: This paper reports on measurements of freestream nitric oxide (NO) rotational and vibrational temperatures and partial pressures, collected in the Caltech T5 reflected shock tunnel. Quantum cascade...
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Keywords:
temperatures partial;
freestream nitric;
reflected shock;
shock tunnel ... See more keywords
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Published in 2021 at "Journal of Thermophysics and Heat Transfer"
DOI: 10.2514/1.t6016
Abstract: This work describes numerical and experimental research in the Indian Hypersonic Shock Tunnel 3 on a blunt cone model and related computation of the facility parameters: nozzle reservoir conditions...
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Keywords:
cone;
surface energy;
shock;
gas surface ... See more keywords