implemented the turbine environment 100 is only one example of a suitable turbine environment and is not intended to suggest any limitation as to the scope of use or functionality of the invention for example the invention may be implemented in an afterburner industrial burner industrial boiler and the like neither should the turbine environment 100 be interpreted as having any dependency or requirement relating to any one or combination of components illustrated in the exemplary operating environment 100 with reference to fig1 an exemplary system for implementing the invention includes electronic module 102 fuel nozzle 104 and combustion chamber 106 the fuel nozzle 104 is mounted to the combustion chamber 106 using conventional means the fuel nozzle 104 is typically made of conducting material and has an inlet section 108 an outlet port 110 that leads into combustion chamber 106 and a center body 112 an ignitor not shown is used to ignite the fuel mixture in the combustion region after the air and fuel are mixed in a pre mix swirler 114 in afterburners the air enters combustion chamber 106 through separate passages and a fuel nozzle passage is used to introduce fuel in the combustion chamber 106 the operation of the turbine is well known and need not be discussed herein the electronic module 102 may be a separate module.