Simulation study of an aero-piston engine with single stage turbocharger

Hai Ying Lin; Xiang Yang Long

Simulation study of an aero-piston engine with single stage turbocharger

Hai Ying Lin^*
, Xiang Yang Long

^*Corresponding author for this work

School of Transportation Science and Engineering

Beihang University

Research output: Contribution to journal › Article › peer-review

11 Scopus citations

Abstract

The method was introduced for setting up simulation model of an aero-piston engine. The simulation model of an engine with single-stage turbocharger was set up, and the ground performance's simulation computation was finished. The simulation results were coincident with the test data. On the basis of the former works, the high altitude performance simulation was conducted, and the results were consistent with the fly test data.

Original language	English
Pages (from-to)	1332-1338
Number of pages	7
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	24
Issue number	6
State	Published - Jun 2009

Keywords

Piston engine
Simulation model
Turbocharger
Unmanned air vehicle

Cite this

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title = "Simulation study of an aero-piston engine with single stage turbocharger",

abstract = "The method was introduced for setting up simulation model of an aero-piston engine. The simulation model of an engine with single-stage turbocharger was set up, and the ground performance's simulation computation was finished. The simulation results were coincident with the test data. On the basis of the former works, the high altitude performance simulation was conducted, and the results were consistent with the fly test data.",

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AU - Long, Xiang Yang

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AB - The method was introduced for setting up simulation model of an aero-piston engine. The simulation model of an engine with single-stage turbocharger was set up, and the ground performance's simulation computation was finished. The simulation results were coincident with the test data. On the basis of the former works, the high altitude performance simulation was conducted, and the results were consistent with the fly test data.

KW - Piston engine

KW - Simulation model

KW - Turbocharger

KW - Unmanned air vehicle

UR - https://www.scopus.com/pages/publications/67650082747

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SN - 1000-8055

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

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ER -

Simulation study of an aero-piston engine with single stage turbocharger

Abstract

Keywords

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