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By Kenneth K. Kuo, Ragini Acharya(auth.)
A hands-on, built-in method of fixing combustion difficulties in diversified components
An figuring out of turbulence, combustion, and multiphase reacting flows is key for engineers and scientists in lots of industries, together with strength genera-tion, jet and rocket propulsion, toxins keep an eye on, hearth prevention and protection, and fabric processing. This booklet deals a hugely functional dialogue of burning habit and chemical tactics happening in diversified fabrics, arming readers with the instruments they should resolve the main complicated combustion difficulties dealing with the medical neighborhood at the present time. the second one of a two-volume paintings, purposes of Turbulent and Multiphase Combustion expands on issues related to laminar flames from Professor Kuo's bestselling booklet ideas of Combustion, moment variation, then builds upon the idea mentioned within the significant other quantity basics of Turbulent and Multiphase Combustion to handle intimately state-of-the-art experimental ideas and functions now not lined wherever else.
Special gains of this booklet contain:
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Coverage of complex functions akin to sturdy propellants, burning habit, and chemical boundary layer flows
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A multiphase platforms strategy discussing easy techniques ahead of relocating to higher-level purposes
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A huge variety of sensible examples gleaned from the authors' event besides difficulties and a ideas manual
Engineers and researchers in chemical and mechanical engineering and fabrics technological know-how will locate purposes of Turbulent and Multiphase Combustion an imperative advisor for upgrading their abilities and maintaining with this speedily evolving zone. it's also a superb source for college kids and pros in mechanical, chemical, and aerospace engineering.Content:
Chapter 1 strong 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 good Propellants (pages 143–208):
Chapter four Chemically Reacting Boundary?Layer Flows (pages 209–329):
Chapter five Ignition and Combustion of unmarried lively strong debris (pages 330–455):
Chapter 6 Combustion of good debris in Multiphase Flows (pages 456–506):
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Additional info for Applications of Turbulent and Multiphase Combustion
Example text
This equation is valid only when the gas cross-flow velocity over the propellant surface is low enough so that shear-induced effects on the burning rate can be ignored. In the case of high-velocity flow of combustion gases over the burning propellant surface, a different equation must be used to include the erosive burning effect. For practical applications, a lower-pressure exponent is considered favorable since that implies relatively uniform burning of solid propellant during pressurization in the solid propellant rocket motor.
17. 31. 0024 K−1 at high pressures. 32 was proposed. 17 Measured burning rates of JA2 propellant at different initial temperatures as a function of pressure (Kuo and Zhang, 2006). 28). This phenomenon is known as slopebreak in burning rate expression, which represents the change in the burning mechanism of the solid propellant from one pressure regime to another. For JA2 propellant with ambient temperature as the initial temperature, its burning rate can be expressed by two different correlations.
According to Louwers (2000), HNF-based propellants could have up to 7% performance gain in comparison with existing AP-based solid propellants. Another advantage is that HNF-based solid propellants do not contain chlorine; therefore, the combustion products of these propellants are more environmentally benign. One of the major drawbacks of HNF is its nonspherical crystalline structure. Also, it is slightly hygroscopic, so special care must be taken during the processing and handling of HNF-based solid propellants.