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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