High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging (open access)

High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging

Report presenting an investigation of 57 experimental tubular designs embodying adjacent fuel-rich and air-rich regions and axial staging of the fuel introduction at simulated high-altitude conditions. Results regarding the development of pilot, development of secondary-air admission sleeve, development of final configuration, and performance of best configuration are provided.
Date: March 22, 1954
Creator: Scull, Wilfred E.
System: The UNT Digital Library