Calculations of the Performance of a Compression-ignition Engine-compressor Turbine Combination PDF Download
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Author: J. C. Sanders Publisher: ISBN: Category : Airplanes Languages : en Pages : 28
Book Description
Small high-speed single-cylinder compression-ignition engines were tested to determine their performance characteristics under high supercharging. Calculations were made on the energy available in the exhaust gas of the compression-ignition engines. The maximum power at any given maximum cylinder pressure was obtained when the compression pressure was equal to the maximum cylinder pressure. Constant-pressure combustion was found possible at an engine speed of 2200 rpm. Exhaust pressures and temperatures were determined from an analysis of indicator cards. The analysis showed that, at rich mixtures with the exhaust back pressure equal to the inlet-air pressure, there is excess energy available for driving a turbine over that required for supercharging. The presence of this excess energy indicates that a highly supercharged compression-ignition engine might be desirable as a compressor and combustion chamber for a turbine.
Author: J. C. Sanders Publisher: ISBN: Category : Airplanes Languages : en Pages : 28
Book Description
Small high-speed single-cylinder compression-ignition engines were tested to determine their performance characteristics under high supercharging. Calculations were made on the energy available in the exhaust gas of the compression-ignition engines. The maximum power at any given maximum cylinder pressure was obtained when the compression pressure was equal to the maximum cylinder pressure. Constant-pressure combustion was found possible at an engine speed of 2200 rpm. Exhaust pressures and temperatures were determined from an analysis of indicator cards. The analysis showed that, at rich mixtures with the exhaust back pressure equal to the inlet-air pressure, there is excess energy available for driving a turbine over that required for supercharging. The presence of this excess energy indicates that a highly supercharged compression-ignition engine might be desirable as a compressor and combustion chamber for a turbine.
Author: Alexander Mendelson Publisher: ISBN: Category : Diesel motor Languages : en Pages : 28
Book Description
Comparison with a compression-ignition engine using a turbosupercharger showed that little could be gained by gearing the turbine to the engine, provided the turbosupercharger could be stably operated with a closed wast gate.
Author: Max A. Heaslet Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 656
Book Description
Under the assumptions of linearized theory, general methods of solutin are given for two- and three-dimensional steady-state and two-dimensional unsteady-state equations of compressible flow. The solutions depend in all cases on the use of Green's equivalent layer of sources, sinks, and doublets. Emphasis is placed on applications in supersonic wing theory, the singularities arising in the integrations being treated by Hadamard's finite part of the technique. Four examples of different character are discussed. In particular, the load distribution over a specific swept-back lifting surface is determined at a free-stream Mach number of one.
Author: Charles Fayette Taylor Publisher: MIT Press ISBN: 9780262700269 Category : Technology & Engineering Languages : en Pages : 588
Book Description
This revised edition of Taylor's classic work on the internal-combustion engine incorporates changes and additions in engine design and control that have been brought on by the world petroleum crisis, the subsequent emphasis on fuel economy, and the legal restraints on air pollution. The fundamentals and the topical organization, however, remain the same. The analytic rather than merely descriptive treatment of actual engine cycles, the exhaustive studies of air capacity, heat flow, friction, and the effects of cylinder size, and the emphasis on application have been preserved. These are the basic qualities that have made Taylor's work indispensable to more than one generation of engineers and designers of internal-combustion engines, as well as to teachers and graduate students in the fields of power, internal-combustion engineering, and general machine design.
Author: J. C. Sanders
Author: J. C. Sanders
Author: Alexander Mendelson
Author: Alexander Mendelson
Author: Alexander Mendelson
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: Max A. Heaslet
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: Charles Fayette Taylor