A study on the high stability control for the integrated aero-propulsion system under supersonic state-Reference-Cited by-同舟云学术

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A study on the high stability control for the integrated aero-propulsion system under supersonic state

Published:2018-05 Issue: Volume:76 Page:350-360
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sun Fengyong,Li Yongjin,Du Yao,Zhang Haibo

Funder

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Aero-engine cycle parametric analysis and installed performance calculation based on aircraft flight mission;Zhou;Appl. Mech. Mater.,2014

2. Aircraft engine performance study using flight data recorder archives;Chati,2013

3. High Stability Engine Control (HISTEC);DeLaat,1996

4. Development and Testing of a High Stability Engine Control (HISTEC) System;Orme,1998

5. High Stability Engine Control (HISTEC) Flight Test Results;Southwick,1998

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