Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand
- Authors: Pogorelov G.I.1, Krivosheev I.A.2, Godovanyuk A.G.2, Danilin O.E.2, Badamshin B.I.2
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Affiliations:
- Open joint-stock company ufa's research-and-production enterprise «Molniya»
- Ufa's state aircraft technical university
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 217-226
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6813
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-217-226
- ID: 6813
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Abstract
There was shown offered method’s of linear interpolation propfan’s multidimensional characteristic results using for modeling turboprofan jet in a total range of flight conditions and approach to equivalent specific fuel consumption optimization subsystem construction in automatic control system structure for reduction of environmental tests and maintenance costs. The offered methods considers requirements to mathematical models for the seminatural modeling stand - simplicity, ensuring of sufficient accuracy of result, work and functioning engine’s mathematical model in a mode of real time.
About the authors
G. I. Pogorelov
Open joint-stock company ufa's research-and-production enterprise «Molniya»
Author for correspondence.
Email: pogorelov@molniya-ufa.ru
candidate of technical sciences
general director deputy
I. A. Krivosheev
Ufa's state aircraft technical university
Email: krivosh@sci.ugatu.ac.ru
doctor of technical sciences, professor
Russian FederationA. G. Godovanyuk
Ufa's state aircraft technical university
Email: algen82@mail.ru
junior researcher
Russian FederationO. E. Danilin
Ufa's state aircraft technical university
Email: odanilin@mail.ru
candidate of technical sciences, associate professor
Russian FederationB. I. Badamshin
Ufa's state aircraft technical university
Email: badbul_auto@inbox.ru
post-graduate student
Russian Federation