Get Applications of Turbulent and Multiphase Combustion PDF

By Kenneth K. Kuo, Ragini Acharya(auth.)

ISBN-10: 1118127560

ISBN-13: 9781118127568

ISBN-10: 1118127579

ISBN-13: 9781118127575

A hands-on, built-in method of fixing combustion difficulties in different parts

An realizing of turbulence, combustion, and multiphase reacting flows is vital for engineers and scientists in lots of industries, together with strength genera-tion, jet and rocket propulsion, pollutants regulate, hearth prevention and safeguard, and fabric processing. This ebook bargains a hugely useful dialogue of burning habit and chemical procedures taking place in different fabrics, arming readers with the instruments they should resolve the main advanced combustion difficulties dealing with the medical group this day. the second one of a two-volume paintings, purposes of Turbulent and Multiphase Combustion expands on issues concerning laminar flames from Professor Kuo's bestselling publication rules of Combustion, moment version, then builds upon the idea mentioned within the better half quantity basics of Turbulent and Multiphase Combustion to handle intimately state-of-the-art experimental strategies and functions no longer coated wherever else.

Special gains of this e-book contain:

  • Coverage of complicated functions comparable to stable propellants, burning habit, and chemical boundary layer flows

  • A multiphase structures technique discussing easy techniques sooner than relocating to higher-level functions

  • A huge variety of functional examples gleaned from the authors' event in addition to difficulties and a strategies manual

Engineers and researchers in chemical and mechanical engineering and fabrics technology will locate purposes of Turbulent and Multiphase Combustion an critical consultant for upgrading their abilities and maintaining with this speedily evolving sector. it's also a superb source for college kids and pros in mechanical, chemical, and aerospace engineering.Content:
Chapter 1 reliable Propellants and their Combustion features (pages 1–71):
Chapter 2 Thermal Decomposition and Combustion of Nitramines (pages 72–142):
Chapter three Burning habit of Homogeneous strong Propellants (pages 143–208):
Chapter four Chemically Reacting Boundary?Layer Flows (pages 209–329):
Chapter five Ignition and Combustion of unmarried full of life good debris (pages 330–455):
Chapter 6 Combustion of good debris in Multiphase Flows (pages 456–506):

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Extra info for Applications of Turbulent and Multiphase Combustion

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Commercial applications include, among others, rockets for space explorations, satellite deployment, air bags in automobiles, electric cable connections, emergency airplane crew and passenger escape systems, gas generator systems for fire extinguishers. 3) determines the method of labeling and the cost of shipping rocket propellants, loaded military missiles, explosives, or ammunition; it also determines the required limits on the amount of that propellant stored or manufactured in any one site and the minimum separation distance of that site to the next building or site.

16b. 16c. In spite of these multi-dimensional effects at the surface, the overall regression process still can be close to a one-dimensional process. M. C. 15 burner. 16 (b) JA2 Propellant (c) M43 Propellant Close-up view of the surface burning behavior of three different propellants. 28 SOLID PROPELLANTS AND THEIR COMBUSTION CHARACTERISTICS the fuel under high-pressure conditions, thereby making the surface nonflat, which introduces multidimensional effects. 1 Measured and Correlated Burning Rates of JA2 Propellant Combustion characteristics of JA2 propellant were studied both experimentally and theoretically by Kuo and Zhang (2006), who investigated the steady-state burning behavior was investigated by using an optical strand burner.

11 Ti Thermal wave thicknesses in a burning solid propellant. 11), we have T − Ti ry dT =− s exp − b dy αp /rb αp or dT dy =− y=0 Ts − Ti αp /rb The physical meaning of the term (αp /rb ) represents a depth at which the tangent line to the temperature profile intersects with the initial temperature profile (T = Ti = constant). 6 defined by the tangent line method is simply the ratio of the thermal diffusivity of solid propellant αp to its burning rate rb . 368. Although this is not the full thermal wave depth, it is referred in the solid propellant literature as the thermal wave depth, δth .

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Applications of Turbulent and Multiphase Combustion by Kenneth K. Kuo, Ragini Acharya(auth.)


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