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: | Monograph (Technical Report) |
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Uncontrolled Keywords: | C program;Jet engine cycles |
Subjects: | MATHEMATICAL AND COMPUTER SCIENCES > Computer Programming and Software |
Depositing User: | Mr. Ravikumar R |
Date Deposited: | 02 Jun 2006 |
Last Modified: | 24 May 2010 04:13 |
URI: | http://nal-ir.nal.res.in/id/eprint/1691 |
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