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タイトルThe Navy/NASA Engine Program (NNEP89): A user's manual
本文(外部サイト)http://hdl.handle.net/2060/19910020827
著者(英)Snyder, Christopher A.; Plencner, Robert M.
著者所属(英)NASA Lewis Research Center
発行日1991-08-01
言語eng
内容記述An engine simulation computer code called NNEP89 was written to perform 1-D steady state thermodynamic analysis of turbine engine cycles. By using a very flexible method of input, a set of standard components are connected at execution time to simulate almost any turbine engine configuration that the user could imagine. The code was used to simulate a wide range of engine cycles from turboshafts and turboprops to air turborockets and supersonic cruise variable cycle engines. Off design performance is calculated through the use of component performance maps. A chemical equilibrium model is incorporated to adequately predict chemical dissociation as well as model virtually any fuel. NNEP89 is written in standard FORTRAN77 with clear structured programming and extensive internal documentation. The standard FORTRAN77 programming allows it to be installed onto most mainframe computers and workstations without modification. The NNEP89 code was derived from the Navy/NASA Engine program (NNEP). NNEP89 provides many improvements and enhancements to the original NNEP code and incorporates features which make it easier to use for the novice user. This is a comprehensive user's guide for the NNEP89 code.
NASA分類AIRCRAFT PROPULSION AND POWER
レポートNO91N30141
NASA-TM-105186
E-6484
NAS 1.15:105186
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/131263


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