Author: Azzedine MissoumPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Atomization of Liquid Fuels in Supersonic Flow
Author: Azzedine MissoumThe Atomisation of Liquid Fuels
Author: Edmund GiffenPublisher:
ISBN:
Category : Science
Languages : en
Pages : 288
Book Description
Atomization of Liquid Fuels
Author: Dr. KuehnPublisher:
ISBN:
Category : Atomization
Languages : en
Pages : 784
Book Description
Atomization of a Liquid in a Supersonic Flow
Author: M. S. VolynskiiPublisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
The development of the process of combustion in a high temperature supersonic flow is determined by the quality of the fuel atomization, in the engine atomization, evaporation, and mixing. The results of a study of the form of the torch of atomization and also the scale of the atomization in a supersonic flow are presented. An examination of the process of atomization is conducted within the frame work of an aerodynamically posed problem without a computation of the heat transfer and phase transitions (evaporation, dissociation etc.) It is assumed that disintegration of the liquid occurs very rapidly and the heat phenomena (in a number of cases do not succeed in influencing substantially the initial diameter of the particles (which later on, of course, are subject to evaporation).
The Atomization of Liquid and Two-Phase Flows
Author: M. S. VolynskiiPublisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
The theory of the spraying of a liquid fuel into a supersonic gaseous stream and of the flow of the dispersed liquid is examined. Systems of equations are presented for 2 phase flow at the initial and main portions of the stream. These equations were solved with a computer and the region of vaporization of the fuel into the supersonic jet was determined. Calculations for streams at Mach 2 are in good agreement with expectations. (Author).
Jet in Supersonic Crossflow
Author: Mingbo SunPublisher: Springer
ISBN: 9811360251
Category : Technology & Engineering
Languages : en
Pages : 284
Book Description
Based on research into jets in supersonic crossflow carried out by the authors’ team over the past 15 years, this book summarizes and presents many cutting-edge findings and analyses on this subject. It tackles the complicated mixing process of gas jets and atomization process of liquid jets in supersonic crossflow, and studies their physical mechanisms. Advanced experimental and numerical techniques are applied to further readers’ understanding of atomization, mixing, and combustion of fuel jets in supersonic crossflow, which can promote superior fuel injection design in scramjet engines. The book offers a valuable reference guide for all researchers and engineers working on the design of scramjet engines, and will also benefit graduate students majoring in aeronautical and aerospace engineering.
Investigation of Liquid Hydrocarbon Combustion in Supersonic Flow Using Effervescent Atomization
Author: G. YuLiquid Atomization in Supersonic Flows
Author: Azzedine MissoumInjection, Atomization, Ignition and Combustion of Liquid Fuels in High-Speed Air Streams
Author: Joseph A. SchetzPublisher:
ISBN:
Category :
Languages : en
Pages : 25
Book Description
Experimental studies of the penetration, break-up and atomization of transverse liquid and slurry jets were performed. All tests were with an air cross flow at Mach 3.0 with Po = 4 atm. and To = 300 deg K. The processes studied were: (1) the effects of injectant viscosity and surface tension, (2) the performance of an impinging jet injector and (3) the effects of particle loading for a slurry jet with 3-50 micrometer particles. The diffractively scattered light method was employed at these high-density, supersonic conditions to study droplet sizes. The major results are, (1) mean droplet size is approximately 10 microns for injectors of 0.05 in., (2) it has an inverse relation with jet/free stream dynamic pressure ratio, (3) it has a direct relation with orifice diameter, (4) it decreases downstream, (5) transverse variation has no simple pattern and (6) droplet size increases with viscosity.
Author: