NASA NTRS · 19880000114
Computer Code For Turbocompounded Adiabatic Diesel Engine
Abstract
Computer simulation developed to study advantages of increased exhaust enthalpy in adiabatic turbocompounded diesel engine. Subsytems of conceptual engine include compressor, reciprocator, turbocharger turbine, compounded turbine, ducting, and heat exchangers. Focus of simulation of total system is to define transfers of mass and energy, including release and transfer of heat and transfer of work in each subsystem, and relationship among subsystems. Written in FORTRAN IV.
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Assanis, D. N., Heywood, J. B.. 1988-02-01. Computer Code For Turbocompounded Adiabatic Diesel Engine. https://ntrs.nasa.gov/citations/19880000114
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