Reference health
Experimental study on the thermodynamic characteristics of the high temperature hydrocarbon fuel in the cooling channel of the hypersonic vehicle
35/35 checkable references clean · checked 2026-07-23
Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.
5 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.
The 35 checked references that resolve
resolves10.1016/j.applthermaleng.2016.04.117
Investigation on thermal and thermomechanical performances of actively cooled corrugated sandwich structures
resolves10.1177/0954410013479730
Hydrogen-fueled scramjet cooling system investigation using combustor and regenerative cooling coupled model
resolves10.2514/2.5895
Upper Bounds on the Flight Speed of Hydrocarbon-Fueled Scramjet-Powered Vehicles
resolves10.2514/1.B36866
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios
resolves10.1016/j.applthermaleng.2017.03.062
Flow and thermal analyses of regenerative cooling in non-uniform channels for combustion chamber
resolves10.1016/j.applthermaleng.2015.12.088
Numerical investigation of flow distribution and heat transfer of hydrocarbon fuel in regenerative cooling panel
resolves10.1016/j.expthermflusci.2018.03.030
Research on heat transfer characteristics of kerosene at supercritical pressure in circular tubes
resolves10.1021/acs.energyfuels.8b00531
Thermal Cracking of Endothermic Hydrocarbon Fuel in Regenerative Cooling Channels with Different Geometric Structures
resolves10.1016/j.applthermaleng.2016.12.074
The comprehensive study on hydrocarbon fuel pyrolysis and heat transfer characteristics
resolves10.1016/j.combustflame.2017.09.033
A composite-fuel additive design method for n-decane low-temperature ignition enhancement
resolves10.1016/j.applthermaleng.2017.05.038
Experimental investigation on thermal-hydraulic characteristics of endothermic hydrocarbon fuel in 1 mm and 2 mm diameter mini-channels
resolves10.1016/j.jaap.2017.08.009
Molecular-level modeling investigation of n-decane pyrolysis at high temperature
resolves10.1016/j.jppr.2015.10.002
Model validation and parametric study of fluid flows and heat transfer of aviation kerosene with endothermic pyrolysis at supercritical pressure
resolves10.2514/1.T4704
Flight Acceleration Effect on Heat Transfer Deterioration of Actively Cooled Scramjet Engines
resolves10.1016/j.cja.2018.03.015
Numerical investigation of pyrolysis effects on heat transfer characteristics and flow resistance of n-decane under supercritical pressure
resolves10.1016/j.ijheatmasstransfer.2018.01.089
Large eddy simulation of supercritical heat transfer to hydrocarbon fuel
resolves10.1016/j.ijheatmasstransfer.2015.07.118
Numerical investigation of heat transfer characteristics and flow resistance of kerosene RP-3 under supercritical pressure
resolves10.1115/1.4037086
Flow and Heat Transfer Characteristics of Supercritical Hydrocarbon Fuel in Mini Channels With Dimples
resolves10.2514/1.B35563
Thermal Behavior Inside Scramjet Cooling Channels at Different Channel Aspect Ratios
resolves10.1016/j.actaastro.2016.05.015
Thermal behavior in the cracking reaction zone of scramjet cooling channels at different channel aspect ratios
resolves10.1016/j.applthermaleng.2015.08.033
Dynamic behaviors of coking process during pyrolysis of China aviation kerosene RP-3
resolves10.2514/1.B35694
Heat Transfer of Hydrocarbon Fuel Under Steady States and Pressure-Transient States
resolves10.1016/j.ijheatmasstransfer.2017.12.057
Experimental investigation of the flow and heat transfer instabilities in n-decane at supercritical pressures in a vertical tube
resolves10.1016/j.actaastro.2015.08.009
Experimental investigation on the onset of thermo-acoustic instability of supercritical hydrocarbon fuel flowing in a small-scale channel
resolves10.1021/je200523a
Isobaric Specific Heat Capacity Measurement for Kerosene RP-3 in the Near-Critical and Supercritical Regions
resolves10.1021/je200258g
Density Measurements of Endothermic Hydrocarbon Fuel at Sub- and Supercritical Conditions
resolves10.1007/s10765-015-1840-4
Thermal-Conductivity Measurements of Aviation Kerosene RP-3 from (285 to 513) K at Sub- and Supercritical Pressures
resolves10.1021/je200901y
Viscosity Measurements of Endothermic Hydrocarbon Fuel from (298 to 788) K under Supercritical Pressure Conditions
The 5 references without a DOI — listed, not checked
no DOI — not checkedReview of the potential of silanes as Rocket/Scramjet fuels
no DOI — not checked10.1016/j.actaastro.2018.11.021_bib10
no DOI — not checkedNational Institute of Standards and Technology Webbook, <http://webbook.nist.gov/chemistry/fluid/>.
no DOI — not checked10.1016/j.actaastro.2018.11.021_bib19
no DOI — not checked10.1016/j.actaastro.2018.11.021_bib20
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