Author: G. YuPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Investigation of Liquid Hydrocarbon Combustion in Supersonic Flow Using Effervescent Atomization
Author: G. YuExperimental Investigation of Supersonic Combustion of Liquid Hydrocarbon Fuel Using Barbotage in the Aeroramp Configuration at M
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
This report results from a contract tasking TsAGl as follows: The contractor will investigate combustion of kerosene using barbotage by hydrogen and air in the aeroramp configuration at M=2.5 as described in his proposal dated 1 Jun 98.
Ignition and Combustion of Liquid Hydrocarbon Fuels in Supersonic Flow
Author: Simon SlutskyPublisher:
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.
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit: 02-4250 - 02-4299
Author: 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).
Investigation of Supersonic Combustion of Hydrocarbon Fuel-rich Hot Gas in Scramjet Combustor
Author: M. SituScramjet Propulsion
Author: Dora MusielakPublisher: John Wiley & Sons
ISBN: 1119640601
Category : Technology & Engineering
Languages : en
Pages : 516
Book Description
Scramjet Propulsion Explore the cutting edge of HAP technologies with this comprehensive resource from an international leader in her field Scramjet Propulsion: A Practical Introduction delivers a comprehensive treatment of hypersonic air breathing propulsion and its applications. The book covers the most up-to-date hypersonic technologies, like endothermic fuels, fuel injection and flameholding systems, high temperature materials, and TPS, and offers technological overviews of hypersonic flight platforms like the X-43A, X-51A, and HiFIRE. It is organized around easy-to-understand explanations of technical challenges and provides extensive references for the information contained within. The highly accomplished author provides readers with a fulsome description of the theoretical underpinnings of hypersonic technologies, as well as critical design and technology issues affecting hypersonic air breathing propulsion technologies. The book’s combination of introductory theory and advanced instruction about individual hypersonic engine components is ideal for students and practitioners in fields as diverse as hypersonic vehicle and propulsion development for missile defense technologies, launch aerospaceplanes, and civilian transports. Over 250 illustrations and tables round out the material. Readers will also learn from: A thorough introduction to hypersonic flight, hypersonic vehicle concepts, and a review of fundamental principles in hypersonic air breathing propulsion Explorations of the aerothermodynamics of scramjet engines and the design of scramjet components, as well as hypersonic air breathing propulsion combustors and fuels Analyses of dual-mode combustion phenomena, materials structures, and thermal management in hypersonic vehicles, and combined cycle propulsion An examination of CFD analysis, ground and flight testing, and simulation Perfect for researchers and graduate students in aerospace engineering, Scramjet Propulsion: A Practical Introduction is also an indispensable addition to the libraries of engineers working on hypersonic vehicle development seeking a state-of-the-art resource in one of the most potentially disruptive areas of aerospace research today.
Investigation of Fuel Injection and Flame Stabilization in Liquid Hydrocarbon-fueled Supersonic Combustors
Author: G. YuScientific and Technical Aerospace Reports
Author: Experimental and Numerical Investigation of Hydrogen Combustion in a Supersonic Flow
Author: Corin SegalPublisher:
ISBN:
Category : Combustion engineering
Languages : en
Pages : 324
Book Description