A SIMPLIFIED METHOD OF TRANSIENT MATHEMATICAL MODEL FOR NON-AUGMENTATION ENGINE

Yu Weifeng; Zhang Shaoji

Volume 7 Issue 1

Jan. 1992

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Article Navigation > Journal of Aerospace Power > 1992 > 7(1): 92-94,102

Yu Weifeng, Zhang Shaoji. A SIMPLIFIED METHOD OF TRANSIENT MATHEMATICAL MODEL FOR NON-AUGMENTATION ENGINE[J]. Journal of Aerospace Power, 1992, 7(1): 92-94,102.

Citation:

Yu Weifeng, Zhang Shaoji. A SIMPLIFIED METHOD OF TRANSIENT MATHEMATICAL MODEL FOR NON-AUGMENTATION ENGINE[J]. Journal of Aerospace Power, 1992, 7(1): 92-94,102.

Yu Weifeng, Zhang Shaoji. A SIMPLIFIED METHOD OF TRANSIENT MATHEMATICAL MODEL FOR NON-AUGMENTATION ENGINE[J]. Journal of Aerospace Power, 1992, 7(1): 92-94,102.

Citation:

Yu Weifeng, Zhang Shaoji. A SIMPLIFIED METHOD OF TRANSIENT MATHEMATICAL MODEL FOR NON-AUGMENTATION ENGINE[J]. Journal of Aerospace Power, 1992, 7(1): 92-94,102.

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A SIMPLIFIED METHOD OF TRANSIENT MATHEMATICAL MODEL FOR NON-AUGMENTATION ENGINE

Shenyang Aeroengine Research Institute

Received Date: 1991-04-01
Publish Date: 1992-01-28

Abstract

Abstract

A simplified method of transient mathematical model for non augmentation engine is presented,which is used in real time simulation for developing engine control system.Two spool inertias are considered in the simplified model,which are the main factors for engine transient performance.