Influence of Engine Parameters on the Power-Unit Performance in Supersonic Aircraft

Siluyanova, M. V.; Kuritsyna, V. V.; Alendar, A. D.; Grunin, Andrey

doi:10.3103/s1068798x20120187

Russ. Engin. Res.

2020

DOI: 10.3103/s1068798x20120187

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Influence of Engine Parameters on the Power-Unit Performance in Supersonic Aircraft

M. V. Siluyanova

V. V. Kuritsyna

A. D. Alendar

et al.

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Cited by 7 publications

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

Alendar¹,

Lanshin²,

Evstigneev³

et al. 2023

VESTNIK of Samara University. Aerospace and Mechanical Engineer

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The problems of creating a propulsion system for a new generation supersonic passenger aircraft are considered on the basis of a review of the work on the supersonic transport being carried out in the world. It is shown that the desire to achieve high flight performance and commercial effectiveness of a supersonic passenger aircraft while meeting up-to-date environmental requirements leads to contradictory technical solutions regarding the propulsion system: the location and number of engines, the scheme of the air intake and nozzle, the choice of the scheme and design parameters of the engine, the use of new high-temperature materials in the engine hot section, etc. The features of the operating conditions of the engine components of a supersonic passenger aircraft in comparison with the engines of up-to-date subsonic civil aviation aircraft and supersonic military aircraft are indicated. The calculated estimates of the influence of various technical solutions on the parameters of the supersonic passenger aircraft engine are given. Due to the complexity and multi-criterion nature of the task of creating a supersonic passenger aircraft propulsion system, its solution requires an integrated approach based on close cooperation of specialists in airframe aerodynamics, engine, etc.

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

Alendar¹,

Lanshin²,

Evstigneev³

et al. 2023

VESTNIK of Samara University. Aerospace and Mechanical Engineer

Self Cite

View full text Add to dashboard Cite

show abstract

Simulation Model of a Propulsion System of a Supersonic Aircraft

Alendar

Siluyanova

2021

Russ. Engin. Res.

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Engineering Model of a Plug Nozzle for the Engine of a Prospective Supersonic Civilian Airplane

2021

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Influence of Engine Parameters on the Power-Unit Performance in Supersonic Aircraft

Cited by 7 publications

References 5 publications

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

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

Simulation Model of a Propulsion System of a Supersonic Aircraft

Engineering Model of a Plug Nozzle for the Engine of a Prospective Supersonic Civilian Airplane

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