Propulsion and Power Plants
Аuthors
Turaevo Engineering Design Bureau «Soyuz», 140080, Moscow region, Lytkarino city, Turaevo I.Z. , building №10
e-mail: lythilkevich@yandex.ru
Abstract
An evaluation of nozzle losses for a liquid fuel ramjet is carried out by means of CFD-simulation techniques. It is demonstrated that radial temperature non-uniformity for a nozzle input causes increasing of values for flow and impulse coefficients onKeywords:
CFD-simulation; ramjet; liquid fuel; nozzle; temperature non-uniformity
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