A Study on Counter Rotating Turbine/Counter Rotating Propfan Integrated Performance Simulation Methodology
Author:
Affiliation:
1. AECC Hunan Aviation Powerplant Research Institute,Zhuzhou,China
2. Wuxi University,Wuxi,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10490442/10490456/10490937.pdf?arnumber=10490937
Reference10 articles.
1. Preliminary Design and Performance of Counter Rotating Turbines for Open Rotors: Part II — 0-D Methodology and Case Study for a 160 PAX Aircraft
2. Model of open rotor engine for aircraft conceptual design;Zhang;Journal of Aerospace Power,2012
3. Research on Open Rotor Engine Calculating Model and Control Schedule;Tu;Aeroengine,2016
4. Modeling and Assessment of a Contra-Rotating Puller Propfan engine;WAng;Journal of Propulsion Technology,2018
5. Wind tunnel performance results of an aero-lastically scaled 2/9 model of the PTA flight test prop-fan;Geroge,29-July 02, 1987
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