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Enhancing the Supersonic Wind Tunnel Performance Based on Plenum Temperature Control
Author(s) -
Amin Nazarian Shahrbabaki,
Mehrdad Bazazzadeh,
Ali Shahriari,
Mojtaba Dehghan Manshadi
Publication year - 2014
Publication title -
isrn aerospace engineering
Language(s) - English
Resource type - Journals
ISSN - 2314-6427
DOI - 10.1155/2014/317049
Subject(s) - plenum space , wind tunnel , supersonic speed , pid controller , control theory (sociology) , temperature control , controller (irrigation) , aerodynamics , nonlinear system , control engineering , engineering , matlab , control system , computer science , mechanical engineering , aerospace engineering , control (management) , physics , operating system , electrical engineering , agronomy , quantum mechanics , artificial intelligence , biology
The application of fuzzy logic controllers (FLCs) to the control of nonlinear processes, typically controlled by a human operator, is a topic of much study. In this paper, the design and application of a FLC is discussed to control the plenum chamber temperature for a blowdown supersonic wind tunnel (BSWT) with the aim of achieving the accurate and desired results. In this regard, first, a nonlinear mathematical model of special BSWT is developed in Matlab/Simulink software environment. Next, an artificially intelligent controller is designed using fuzzy logic approach. For this purpose, a proportional-derivative FLC (PD-FLC) system is developed in the Simulink toolbox to control the plenum stagnation temperature using a heater upstream of the plenum chamber. Finally, the system simulation results inside of the temperature and pressure controllers in comparison with the experimental run are presented. The results for Mach 2.5 blowdown run show the great performance of the Wind Tunnel Simulator Model and its temperature controller system.

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