By James O. Maloney
ISBN-10: 0071511245
ISBN-13: 9780071511247
Now in its 8th version, Perry's Chemical Engineers' instruction manual bargains unmatched, up to date assurance of all facets of chemical engineering. For the 1st time, person sections can be found for buy. you can now obtain basically the content material you would like for a fragment of the cost of the whole quantity. Streamline your examine, pinpoint really expert details, and economize through ordering unmarried sections of this definitive chemical engineering reference this present day.
First released in 1934, Perry's Chemical Engineers' guide has outfitted generations of engineers and chemists with knowledgeable resource of chemical engineering details and information. Now up to date to mirror the newest know-how and approaches of the recent millennium, the 8th version of this vintage advisor presents unsurpassed assurance of each element of chemical engineering-from basic ideas to chemical methods and kit to new desktop purposes.
packed with over seven-hundred precise illustrations, the 8th version of Perry's Chemical Engineers' instruction manual features:
*Comprehensive tables and charts for unit conversion
*A significantly accelerated part on actual and chemical facts
*New to this variation: the most recent advances in distillation, liquid-liquid extraction, reactor modeling, organic techniques, biochemical and membrane separation tactics, and chemical plant safeguard practices with twist of fate case histories
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Additional info for Perry's chemical Engineer's handbook, Section 1
Example text
Liquid hydrazine (N2H4) decomposes exothermicaily in a monopropellant rocket operating at 100 atm chamber pressure. The products formed in the chamber are N2, H2, and ammonia (NH3) according to the irreversible reaction N2H4(liq) -> aN2 + bH2 + CNH3 Determine the adiabatic decomposition temperature and the product composition a, ft, and c. 07 kJ/mol. The hydrazine enters the system at 298 K. 13. Gaseous hydrogen and oxygen are burned at 1 atm under the rich conditions designated by the following combustion reaction: O2 + 5H2 ~> aH20 + 6H2 + cH The gases enter at 298 K.
5. , and Sawyer, R. , 'The Performance of Chemical Propellants," Chap. 11. Technivision, London, 1970. 6. Reynolds, W. C, "Stanjan," Dep. Mech. , Stanford, California, 1986. 7. , East. States Combust. Inst. , Providence, RI Pap. No. 12 (Nov. 1983). 2 Chemical Kinetics A. INTRODUCTION Flames will propagate through only those chemical mixtures that are capable of reacting quickly enough to be considered explosive. Indeed, the expression "explosive" essentially specifies very rapid reaction. From the standpoint of combustion, the interest in chemical kinetic phenomena has generally focused on the conditions under which chemical systems undergo explosive reaction.
Whether a reaction isfirst-or second-order is particularly important in combustion because of the presence of large radicals that decompose into a stable species and a smaller radical (primarily the hydrogen atom). A prominent combustion example E. PsGUdo-First-Order Reactions and the "Fall-Off"Range is the decay of a paraffinic radical to an olefin and a H atom. The order of such reactions, and hence the appropriate rate constant expression, can change with the pressure. Thus, the rate expression developed from one pressure and temperature range may not be applicable to another range.
Perry's chemical Engineer's handbook, Section 1 by James O. Maloney
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