Accession Number : ADA295478
Title : Gas Turbine Comparisons Using The Energy Methods,
Corporate Author : NAVAL ACADEMY ANNAPOLIS MD DIV OF ENGINEERING AND WEAPONS
Personal Author(s) : Lopardo, V. J.
PDF Url : ADA295478
Report Date : JUN 1982
Pagination or Media Count : 63
Abstract : Using the energetic methods of the Second Law of Thermodynamics several gas turbine configurations are compared and evaluated. In all cases the primary loss of energy is associated with the combustion process and the exhaust stream. The use of a regenerator reduces the overall energy dissipation.
Descriptors : *GAS TURBINES, THERMODYNAMICS, COMBUSTION, CONFIGURATIONS, LOSSES, STREAMS.
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE