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NACA research on combustors for aircraft gas turbines 1: effects of operating variables on steady-state performance

Description: Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed. Trends depicting the effect of inlet-air pressure, temperature, and velocity and fuel-air ratio on performance characteristics, such as combustion efficiency, maximum temperature rise attainable, pressure loss, and combustor-outlet temperature distribution are described for a variety of turbojet combustors of the liquid-fuel type. These trends are further discussed as effects significant to the… more
Date: October 18, 1950
Creator: Olson, Walter T. & Childs, J. Howard
Partner: UNT Libraries Government Documents Department
open access

Multiplying Lattices

Description: The use of thermally fissionable material in the lattice adds a distributed source of fast neutrons which must be considered in evaluating the problem.
Date: October 18, 1950
Creator: Brown, H.
Partner: UNT Libraries Government Documents Department
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