In this paper, characteristics of turbulent flow and convective heat transfer of supercritical China RP-3 kerosene in a horizontal straight circular tube are studied experimentally, and the validity of Chilton-Colburn analogy is examined. Using a three-stage heating system, experiments are conducted at a fuel temperature range of 650-800 K, a pressure range of 3-4 MPa, and a Reynolds number range of 1 x 10(5) -3.5 x 10(5). The Nusselt number and skin friction coefficient are calculated through control volume analysis proposed in this paper. Heat transfer enhancement and deterioration were observed in the experiments as well as the similar change of skin friction coefficient. The present results show that Chilton-Colburn analogy is also vali...
Turbulent flow and convective heat transfer of kerosene in coiled pipes with different wall boundary...
A new friction-heat transfer analogy for the prediction of heat transfer to turbulent fluids at sup...
The characteristics of flow resistance of a typical hydrocarbon fuel (RP-3) flow through adiabatic h...
The finite volume discrete solution of the Navier-Stokes equation and the RNG model of the turbulenc...
The now and heat transfer characteristics of China No. 3 aviation kerosene in a heated curved tube u...
This study experimentally investigated convective heat transfer performances of China RP-3 kerosene ...
Convective heat transfer of aviation kerosene at supercritical pressures in a vertical upward tube o...
Regenerative cooling of aviation kerosene plays an important role for thermal protection of scramjet...
Convective heat transfer of aviation kerosene at supercritical pressures in a vertical upward tube w...
Purpose - The purpose of this paper is to numerically investigate the heat transfer performance of a...
In order to obtain a deeper understanding of the regenerative cooling process of scramjet engines, i...
In this paper, turbulent flow of aviation kerosene at supercritical pressure through cooling channel...
Purpose: This paper aims to comprehensively clarify the research status of thermal transport of supe...
In the present paper, numerical study of flow and heat transfer properties of RP-3 kerosene at liqui...
In this paper, compressible flow of aviation kerosene at supercritical conditions has been studied b...
Turbulent flow and convective heat transfer of kerosene in coiled pipes with different wall boundary...
A new friction-heat transfer analogy for the prediction of heat transfer to turbulent fluids at sup...
The characteristics of flow resistance of a typical hydrocarbon fuel (RP-3) flow through adiabatic h...
The finite volume discrete solution of the Navier-Stokes equation and the RNG model of the turbulenc...
The now and heat transfer characteristics of China No. 3 aviation kerosene in a heated curved tube u...
This study experimentally investigated convective heat transfer performances of China RP-3 kerosene ...
Convective heat transfer of aviation kerosene at supercritical pressures in a vertical upward tube o...
Regenerative cooling of aviation kerosene plays an important role for thermal protection of scramjet...
Convective heat transfer of aviation kerosene at supercritical pressures in a vertical upward tube w...
Purpose - The purpose of this paper is to numerically investigate the heat transfer performance of a...
In order to obtain a deeper understanding of the regenerative cooling process of scramjet engines, i...
In this paper, turbulent flow of aviation kerosene at supercritical pressure through cooling channel...
Purpose: This paper aims to comprehensively clarify the research status of thermal transport of supe...
In the present paper, numerical study of flow and heat transfer properties of RP-3 kerosene at liqui...
In this paper, compressible flow of aviation kerosene at supercritical conditions has been studied b...
Turbulent flow and convective heat transfer of kerosene in coiled pipes with different wall boundary...
A new friction-heat transfer analogy for the prediction of heat transfer to turbulent fluids at sup...
The characteristics of flow resistance of a typical hydrocarbon fuel (RP-3) flow through adiabatic h...