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Vol 22, No 1 (2023)

The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)

Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.

(Rus)

Vol 23, No 2 (2024)

Comparative results of computational and theoretical study of the annular nozzle with a flat central body

Kirshina A.A., Levikhin A.A., Kirshin A.Y.

(Rus)

Vol 8, No 3-3 (2009): Special Issue

Manipulate pulsed detonation engine

1 1., 1 1.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Mathematical modelling and parametric research of flow of the twisted turbulent single-component stream of the propulsive mass in the trance- and supersonic areas of Laval nozzles

1 1., 1 1.

(Rus)

Vol 20, No 4 (2021)

Parametric study of the influence of location and extension height of the rod interceptor on jet engine nozzle characteristics

Tishchenko K.O., Brykov N.A., Belyaeva A.S.

(Rus)

Vol 8, No 1 (2009)

Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle

Shustov S.A.

(Rus)

Vol 16, No 2 (2017)

Numerical modeling and experimental research of a two-phase liquid- gas ejector with a profiled supersonic nozzle

Lepeshinsky I.A., Reshetnikov V.A., Zarankevich I.A.

(Rus)

Vol 8, No 1 (2009)

Numerical model of viscosity impact on flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with velocity slip

Shustov S.A.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Modelling of an ejector for turbine aeroengines for application in performance synthesis tools

Georgi J., Staudacher S., Falaleev S.V.

(Rus)

Vol 8, No 1 (2009)

Approbation of the numerical model of account of viscosity impact on the flow in low-thrust rocket engine nozzles in the approximation of a laminar boundary layer with sliding

Shustov S.A.

(Rus)

Vol 13, No 1 (2014)

Numerical investigation of gas dynamics in nozzles of small-dimensioned gas generators and flowing out jets

Ivanov I., Kryukov I., Shustov S.

(Rus)

Vol 9, No 2 (2010): Special Issue

Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 9, No 1 (2010)

Dynamic analysis and optimization of turbojet engine nozzle control mechanism

(Rus)

1 - 13 of 13 Items

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