Numerical operability evaluation for an ajustable two-position nozzle

Аuthors

Hilkevich V. Y.

Turaevo Engineering Design Bureau «Soyuz», 140080, Moscow region, Lytkarino city, Turaevo I.Z. , building №10

e-mail: lythilkevich@yandex.ru

Abstract

A mathematical model is suggested for adjustable two-position nozzles intended to liquid fuel ramjets. An example is solved to demonstrate operability of the nozzle both in closed and open positions.

Keywords:

mathematical modelling; ramjet; liquid fuel; adjustable nozzle