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http://dx.doi.org/10.5139/JKSAS.2010.39.3.269

The Performance Modeling of a Low Bypass Turbofan Engine with Afterburner for Supersonic Aircraft  

Choi, Won (한국항공우주산업(주) 고정익선행연구팀)
Lee, Il-Woo (한국항공우주산업(주) 고정익선행연구팀)
Yang, Jun-Ho (한국항공우주산업(주) 고정익선행연구팀)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.39, no.3, 2011 , pp. 269-278 More about this Journal
Abstract
The details of engine manufacturer's engine simulations are generally kept secret and only those parameters that are used for control purposes are accessible to users. Hence, there is often only a limited amount of data accessible for creating a performance model of the engine. The performance modeling of a low bypass turbofan engine for supersonic aircraft is described herein. The Pratt and Whitney F100-PW-229 engine has been employed for low bypass turbofan engine performance modeling. Published data from the open literature are used as initial data for building the F100-PW-229 engine performance model. The unknown components' characteristics were estimated by optimization of parameters using by adaptive random search method and sensitivity analysis with respect to design variables. The engine performance model was evaluated to be properly constructed through the comparison of result of engine performance analysis and engine deck data.
Keywords
Performance Modeling; low Bypass; Turbofan Engine; Gasturb; Engine Performance;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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