Aramid Nanofiber - Functionalized Graphene Electrode for Structural Energy and Power
Abstract
The research instrumentation funds have been used to build a computer-instrumented and computer-controlled experimental apparatus that emulates the combustor a gas turbine engine. This test apparatus will be specifically designed to be capable of emulating nominal and some of the critical anticipated and unanticipated off-nominal transient operating conditions as well as emergency situations in typical combustors of aircraft gas turbine engines. The apparatus also serves as a test bed for early prediction and real-time active control of (emulated) combustion instabilities in aircraft gas turbine engines From the above perspective, the requested instrumentation has supported and will continue to support experimental validation of the results of theoretical research in dynamic data-driven application systems (DDDAS), which include algorithms of: Real-time knowledge extraction from heterogeneous dynamic data in stochastic settings; Reduced-order modeling trained by experimental data of spatio-temporal dynamics; Machine learning and information fusion at multiple scales of space and time; and Uncertainty quantification in real-time prediction and control of combustion instabilities.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 13, 2020
- Accession Number
- AD1106294
Entities
People
- Dimitris C Lagoudas
- Jodie L. Lutkenhaus
Organizations
- Texas Engineering Experiment Station