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Technique of conclusion the direct-flow detonation pulsing engine design to the leader position
- Authors: Safronov V.V.1, Porshnev V.A.1, Zhebrakov A.S.1
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Affiliations:
- JSC «KB Electropribor»
- Issue: Vol 10, No 3-4 (2011): Special Issue
- Pages: 117-126
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6956
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-4(27)-117-126
- ID: 6956
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Abstract
Statement of a hypervector problem of conclusion the direct-flow detonation pulsing engine design to the leader is considered. Generally it is reduced to multicriteria problem of a discrete programming. The method of its decision is offered. The numerical example is resulted.
About the authors
V. V. Safronov
JSC «KB Electropribor»
Author for correspondence.
Email: svv@kbep.ru
Doctor of Scientific Tech, professor
Russian FederationV. A. Porshnev
JSC «KB Electropribor»
Email: pva@kbep.ru
Candidate of Technical Sciences
chief of the research center
A. S. Zhebrakov
JSC «KB Electropribor»
Email: zas@kbep.ru
Design engineer
Russian FederationReferences
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