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Surging and auto-off the helicopter engine at start-up unguided missile from launchers
- Authors: Prokopiev A.L.1, Povetkin O.V.2
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- JSC «Aviaagregat», Samara
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 257-264
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6889
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-257-264
- ID: 6889
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Abstract
The description of the solutions to minimize the negative impact of surging on the stable operation of the engine helicopter, appearing at the entrance to the air intake of the helicopter at the time of launch unguided aircraft rockets (rockets), and is the application in the construction of the visor and perforated stilling.
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About the authors
A. L. Prokopiev
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Author for correspondence.
Email: vepokorp@yandex.ru
post-graduate student
Russian FederationO. V. Povetkin
JSC «Aviaagregat», Samara
Email: mail@aviaagregat.net
leading engineer
Russian FederationReferences
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