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Analysis and optimization of flow and heat transfer performance of active thermal protection channel for hypersonic aircraft
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Outgoing claims: the papers this work cites, builds on, or argues with.
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Materials Property Profiles for Actively Cooled Panels: An Illustration for Scramjet Applications
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Active flow control by a novel combinational active thermal protection for hypersonic vehicles
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Heat transfer performance and flow characteristics of solar air heaters with inclined trapezoidal vortex generators
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Effects of active cooling on the metal thermal protection systems
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Dimensioning of automated regenerative cooling: Setting of high-end experiment
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Overall thermal performances of backward film cooling with simulated surface thermal barrier coatings at various walls
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Numerical investigation on transpiration cooling with coolant phase change under hypersonic conditions
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Effect of recooling cycle on performance of hydrogen fueled scramjet
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3D numerical investigation of trans-critical heat transfer enhancement in regeneration cooling channel with crescent rib
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A review of floc strength and breakage
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Investigation into The Influences of Turbulence Models on Heating Prediction of Hypersonic Inflatable Aerodynamic Decelerator
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Steady-State Temperature Field in a Separator System Featuring Active Thermal Protection with Anisotropic Properties
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Study on influence of forced vibration of cooling channel on flow and heat transfer of hydrocarbon fuel at supercritical pressure
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Transpiration Cooling Experiment for Scramjet Engine Combustion Chamber by High Heat Fluxes
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Experimental and Numerical Studies of Diamond-Shaped Injector in a Supersonic Flow
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A Century of Ramjet Propulsion Technology Evolution
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Numerical Analysis of Convection / Transpiration Cooling
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Numerical analysis of convection/transpiration cooling
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Platelet Devices - Limited Only by One's Imagination
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Application of the Transpiration Cooling Method for Reentry Vehicles
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Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles
inferredcites →https://doi.org/10.3724/sp.j.1077.2013.12466openalex-snapshot
Research Progress on the Application of C/SiC Composites in Scramjet
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Incoming claims: where this work appears in other papers’ reference lists and arguments.
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Transient porous transpiration cooling using a two-phase semi-mixed model
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Influence of Capsule Geometry on Aerodynamic and Aerothermal Characteristics in Hypersonic Flow
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Design and optimization study of discrete inclined ribs enhanced bend tube based on “Diamond” active cooling thermal protection systems of hypersonic aircraft
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Experimental Study on Thermal Protection Performance of an Insulation–Dissipation Structure
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