NUMERICAL INVESTIGATION OF THE EFFECT OF AERODYNAMIC FRAGMENTATION OF CONDENSATE PARTICLES ON THE TWO-PHASE IMPULSE LOSSES IN A SOLID-FUEL ROCKET ENGINE NOZZLE | Zendy

N. N. Dyachenko | Zendy; L. I. Dyachenko | Zendy; Valeriya Sergeevna GUROVA | Zendy; Sofiya Aleksandrovna SINEOKAYA | Zendy

Open Access

NUMERICAL INVESTIGATION OF THE EFFECT OF AERODYNAMIC FRAGMENTATION OF CONDENSATE PARTICLES ON THE TWO-PHASE IMPULSE LOSSES IN A SOLID-FUEL ROCKET ENGINE NOZZLE

Author(s) -

N. N. Dyachenko,

L. I. Dyachenko,

Valeriya Sergeevna GUROVA,

Sofiya Aleksandrovna SINEOKAYA

Publication year - 2017

Publication title -

vestnik tomskogo gosudarstvennogo universiteta matematika i mekhanika

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.246

H-Index - 5

eISSN - 2311-2255

pISSN - 1998-8621

DOI - 10.17223/19988621/45/8

Subject(s) - nozzle , aerodynamics , impulse (physics) , solid fuel rocket , mechanics , specific impulse , aerospace engineering , rocket engine , materials science , ramjet , rocket engine nozzle , liquid propellant rocket , environmental science , physics , combustion , engineering , propulsion , classical mechanics , propellant , chemistry , combustor , organic chemistry

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