I want to measure flame temperature inside a gas turbine combustor with optical access. How do i do that without interacting with the combustor environment?
Which frequency an spatial resolution you need you need?
if you know the temperature in some region of the chamber (ej: freh gases) you can use shadowgraphy and shlieren methods. These give you first and second derivatives of the optical density with space; this density is nearly proportional to temperature because usually pressure have very low impact in the flame. The optical density is proportional to mass density but depends also on composition (though in fuel-air combustions the effect is usually lower than 10%).
Fluorescence methods can give you also information on the temperature local but are far more complex and expensive.