Design and Experimental Study of the Inlet Temperature Distortion Generator

HOU Min-jie; LIU Da-xiang; WANG Hui-ru

Volume 20 Issue 3

Jun. 2005

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HOU Min-jie, LIU Da-xiang, WANG Hui-ru. Design and Experimental Study of the Inlet Temperature Distortion Generator[J]. Journal of Aerospace Power, 2005, 20(3): 361-367.

Citation:

HOU Min-jie, LIU Da-xiang, WANG Hui-ru. Design and Experimental Study of the Inlet Temperature Distortion Generator[J]. Journal of Aerospace Power, 2005, 20(3): 361-367.

HOU Min-jie, LIU Da-xiang, WANG Hui-ru. Design and Experimental Study of the Inlet Temperature Distortion Generator[J]. Journal of Aerospace Power, 2005, 20(3): 361-367.

Citation:

HOU Min-jie, LIU Da-xiang, WANG Hui-ru. Design and Experimental Study of the Inlet Temperature Distortion Generator[J]. Journal of Aerospace Power, 2005, 20(3): 361-367.

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Design and Experimental Study of the Inlet Temperature Distortion Generator

1.
School of Power and Energy,Northwestern Polytechnical University,Xi’an710072,China
2.
School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing100083,China
3.
China Gas Turbine Establishment,Jiangyou621703,China

Received Date: 2004-05-12
Rev Recd Date: 2004-08-03
Publish Date: 2005-06-28

Abstract

Abstract

The Temperature Distortion Generator (TDG) design specifications,design technique and the technology of its fabrication were presented.The TDG was tested and calibrated using a turbojet engine and a turbofan engine.The test results indicate that the specifications of this TDG satisfy the requirements of engine temperature distortion testing.The equipment is highly reliable,controllable and stable.
- aerospace propulsion system,
- temperature distortion generator,
- temperature distortion,
- aerodynamic stability,
- turbofan