Download or read book Calculations of the Performance of a Compression ignition Engine compressor Turbine Combination written by J. C. Sanders and published by . This book was released on 1945 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Calculation of the Performance of a Compression ignition Engine Compressor Turbine Combination II Performance of Complete Combination written by Alexander Mendelson and published by . This book was released on 1947 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Calculations of the Performance of a Compression ignition Engine compressor Turbine Combination written by Alexander Mendelson and published by . This book was released on 1947 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Calculated Performance of a Compression ignition Engine compressor turbine Combination Based on Experimental Data written by Alexander Mendelson and published by . This book was released on 1948 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 1370 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1948 with total page 642 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Application of Green s Theorem to the Solution of Boundary value Problems in Linearized Supersonic Wing Theory written by Max A. Heaslet and published by . This book was released on 1949 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Technical Note written by and published by . This book was released on 1948 with total page 426 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Internal Combustion Engine in Theory and Practice second edition revised Volume 1 written by Charles Fayette Taylor and published by MIT Press. This book was released on 1985-03-19 with total page 588 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Download or read book Wartime Report E written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wartime Report written by and published by . This book was released on 194? with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reproductions of reports, some declassified, of research done at Aircraft Engine Research Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Download or read book A Theoretical Analysis of the Performance of a Diesel Engine compressor turbine Combination for Aircraft written by Eldon W. Hall and published by . This book was released on 1945 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical study was made of a Diesel engine-compressor-turbine combination for aircraft application. The performance characteristics of the compressor and the turbine chosen for the analysis are believed to be attainable on present aircraft equipment. Maximum cylinder pressure, maximum exhaust-gas temperature, and maximum engine speed were limited to values now obtained on spark-ignition engines. The analysis indicates favorable performance characteristics for the proposed power plant for a number of conditions.
Download or read book Continuation to Date of Bibliography of Unclassified Books and Reports on Gas Turbines Jet Propulsion and Rocket Power Plants written by and published by . This book was released on 1949 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NACA Research Memorandum written by and published by . This book was released on 1947 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1949 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Information Pilot written by and published by . This book was released on 1949 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research Memorandum written by and published by . This book was released on 1947 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
