Conclusion
Aerospace propulsion
Archive REF: BM3001 V1
Conclusion
Aerospace propulsion

Author : Marc BOUCHEZ

Publication date: February 10, 2010 | Lire en français

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3. Conclusion

After the general introduction [BM 3 000] , this article has recalled the essential notions of flight (regimes, standard atmosphere...), the aerodynamic and thermodynamic formulas used in propulsion, at the preliminary design stage, as well as the different levels of air and combustion modeling.

The main definitions were discussed: constructive index, dilution rate, specific impulse.

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