'C' Program for Design Point Performance of Jet Engine Cycles

Srinivasa, C (1992) 'C' Program for Design Point Performance of Jet Engine Cycles. Technical Report. National Aerospace Laboratories, Bangalore, India.

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    Abstract

    'C' language is now becoming very popular and so an attempt has been made to use this language in the development of a computer program to calculate the design point performance of jet engine cycles. Thermodynamic13; analysis of gas turbine engine is important during the development of gas turbine engines. This program is developed on a PC under MS-DOS with Turbo-C language.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: C program;Jet engine cycles
    Subjects: MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software
    Division/Department: Computer Support and Services Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 02 Jun 2006
    Last Modified: 24 May 2010 09:43
    URI: http://nal-ir.nal.res.in/id/eprint/1691

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