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Published in 2018 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2018.09.015
Abstract: Abstract In order to extend the range of flight Mach numbers, the variable-geometry inlet equipped with a translating cowl has been proposed. To estimate the effects that the translation of cowl has on the behavior…
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Keywords:
shock train;
inlet;
train;
translating cowl ... See more keywords
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Published in 2017 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2016.11.007
Abstract: Different factors which help to control the shock train in the scramjet isolator and combustor were analyzed via numerical investigations, and were applied to a whole scramjet engine in the working environment. A streamline traced…
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Keywords:
scramjet engine;
shock train;
shock;
combustor ... See more keywords
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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.02.001
Abstract: Abstract The inlet equipped with a translating cowl is confirmed to have the ability of extending the range of flight Mach numbers. Along with the translation of cowl, the performance of inlet and background waves…
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Keywords:
shock train;
dependence characteristic;
background waves;
shock ... See more keywords
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Published in 2019 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.02.022
Abstract: Abstract To investigate the forced oscillations of shock train caused by sinusoidal backpressure perturbations with different amplitudes and frequencies in a hypersonic inlet equipped with translating cowl, numerical simulations have been conducted with the application…
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Keywords:
backpressure;
shock train;
train;
forced oscillation ... See more keywords
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Published in 2017 at "International Journal of Heat and Mass Transfer"
DOI: 10.1016/j.ijheatmasstransfer.2017.06.074
Abstract: Abstract For the Rocket-Based Combined-Cycle (RBCC) engine, the addition of primary rocket jets makes both the flow field and the shock train structure more complicated. In this study, a three-dimensional Detached Eddy Simulation (DES) modeling…
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Keywords:
central strut;
addition;
detached eddy;
shock train ... See more keywords
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Published in 2017 at "Theoretical and Applied Mechanics Letters"
DOI: 10.1016/j.taml.2017.09.005
Abstract: Abstract Shock tubes are devices which are used in the investigation of high speed and high temperature flow of compressible gas. Inside a shock tube, the interaction between the reflected shock wave and boundary layer…
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Keywords:
shock tube;
tube;
inside shock;
shock train ... See more keywords
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Published in 2020 at "Journal of Fluid Mechanics"
DOI: 10.1017/jfm.2020.702
Abstract: Abstract In a back pressured duct with incident shocks, the shock train exhibits violent oscillations or even a rapid movement when it passes through a shock-wave–boundary-layer interaction (SWBLI) region. In this study, the dynamics of…
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Keywords:
incident shocks;
shock train;
analysis;
shock ... See more keywords
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Published in 2019 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410017727028
Abstract: An experimental investigation of the response of an oblique shock train to downstream periodic pressure perturbations was conducted. The oblique shock train is generated in a Mach 2.7 ducted flow and controlled by a downstream…
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Keywords:
oblique shock;
shock train;
pressure;
shock ... See more keywords
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Published in 2017 at "Journal of Propulsion and Power"
DOI: 10.2514/1.b36291
Abstract: Schlieren images and unsteady pressure measurements were collected to explore the response of a shock train to a high-frequency fluctuating backpressure in an isolator. High-frequency excitations (...
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Keywords:
high frequency;
frequency fluctuating;
frequency;
shock train ... See more keywords
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Published in 2017 at "AIAA Journal"
DOI: 10.2514/1.j055333
Abstract: A dataset of normal shock trains in a rectangular cross-section channel has been created from direct numerical simulations in an effort to quantify the impact of inflow confinement ratio on the sho...
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Keywords:
response inflow;
train response;
shock train;
investigation shock ... See more keywords
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Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059302
Abstract: Within a scramjet, the location of the shock train will change as the backpressure changes. When the shock train leading edge moves out from the entrance of the isolator, the engine usually goes in...
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Keywords:
shock train;
train;
train leading;
leading edge ... See more keywords