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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