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Author: Simon Slutsky Publisher: ISBN: Category : Languages : en Pages : 73
Book Description
An experimental study was carried out to investigate the combustion of a liquid hydrocarbon (hexane) injected into a supersonic stream. Injection modes included wall and central injection configurations. Extremely rapid and intense heat release phenomena were obtained. It was concluded that this mode of combustion could be made to compete with that of pure gas phase combustion for many technological applications. A preliminary theoretical model of the combustion mechanism was constructed which accounts for many of the observed phenomena, and which explains the very rapid combustion characteristics.
Author: Simon Slutsky Publisher: ISBN: Category : Languages : en Pages : 73
Book Description
An experimental study was carried out to investigate the combustion of a liquid hydrocarbon (hexane) injected into a supersonic stream. Injection modes included wall and central injection configurations. Extremely rapid and intense heat release phenomena were obtained. It was concluded that this mode of combustion could be made to compete with that of pure gas phase combustion for many technological applications. A preliminary theoretical model of the combustion mechanism was constructed which accounts for many of the observed phenomena, and which explains the very rapid combustion characteristics.
Author: Vincent J. Siminski Publisher: ISBN: Category : Languages : en Pages : 242
Book Description
The purpose of this program was to determine, analytically and experimentally the extent to which the autoignition delay times of liquid hydrocarbons could be reduced by modification of the molecular structure or through the utilization of homogeneous additives and heterogeneous catalysts. To this end the autoignition delays of a number of different hydrocarbons were determined in three different experimental apparatus; a well-stirred reactor, a constant flow subsonic duct and a supersonic detached jet or ducted flow system. At one atmosphere pressure the velocity and temperature of the test devices were varied from subsonic to supersonic and from 300 to 1600 K respectively. No quantitative relationship could be established between the ignition lags measured in the constant flow system and the average residence times determined in the stirred reactor at the blow-out point. However, it is clear that the stirred reactor data more closely describe the total hydrocarbon combustion time than any 'pseudo ignition lag' associated with the hydrocarbon. Of the more than 25 different homogeneous additives tested, the strongest ignition promoters, by far, were found to be the alkyl nitrates and nitrites or nitric oxide and nitrogen dioxide. The presence of a platinum surface on the walls of the combustion chamber reduced the autoignition temperature of various hydrocarbons by 350 K. Fuel blends consisting of 15 volume percent n-propyl nitrate in either H-MCPD or Shelldyne-H were ignited and combusted in a piloted supersonic flow (Mach 1.5) over a temperature range of 300 to 1300 K.
Author: Publisher: ISBN: Category : Languages : en Pages : 150
Book Description
This report results from a contract tasking Institute of High Temperatures RAS as follows: The contractor will investigate the phenomena of plasma-induced ignition of high speed, low temperature air-fuel mixtures using a recirculation zone created by a rearward facing wall step and wall cavity. The plasma will be generated using a multi-electrode, quasi direct-current electrical discharge. Fuel injectors will be located in the recirculation zone. The effects of plasma induced ignition, mixing intensification, flame-stabilization, and combustion completeness will be evaluated. Investigations will be carried out using both gaseous and liquid hydrocarbon fuels. Diagnostics include high speed video, Schlieren photography, pressure distribution measurements, electrical measurements, optical spectroscopy and infrared absorption spectroscopy. The research is mainly experimental, but will include several analytical and computational efforts for better understanding and verification of the results.
Author: Mingbo Sun Publisher: Springer Nature ISBN: 9811535957 Category : Technology & Engineering Languages : en Pages : 380
Book Description
This book describes the unsteady phenomena needed to understand supersonic combustion. Following an initial chapter that introduces readers to the basic concepts in and classical studies on unsteady supersonic combustion, the book highlights recent studies on unsteady phenomena, which offer insights on e.g. interactions between acoustic waves and flames, flow dominating instability, ignition instability, flame flashback, and near-blowout-limit combustion. In turn, the book discusses in detail the fundamental mechanisms of these phenomena, and puts forward practical suggestions for future scramjet design.
Author: Publisher: ISBN: Category : Languages : en Pages : 139
Book Description
This report results from a contract tasking Moscow State University as follows: The contractor will investigate the use of pulsed plasma jets and transversal pulsed-periodic discharges to ignite and efficiently combust hydrocarbon fuel/air mixtures in supersonic flows. Effects of pulse duration pulse power. electrode material and operating frequency will be determined for both propane/air and kerosene/air mixtures over equivalence rations from 0.3 to 1.0 at Mach 1.5, 2.0 and 3.0. Diagnostics will be used to determine the radiation spectra for the different discharges in the supersonic flow. Measurements of chemical radical and electron concentrations will also be made. Corresponding numerical simulations will be compared to the experimental data.
Author: Simon Slutsky
Author: Simon Slutsky
Author: Vincent J. Siminski
Author: 
Author: Paul David Rudolph
Author: United States. Air Force. Office of Aerospace Research
Author: Mingbo Sun
Author: 
Author: G. Yu
Author: Lewis Flight Propulsion Laboratory. Propulsion Chemistry Division
Author: