Low-Pressure Performance of a Tubular Combustor With Gaseous Hydrogen (open access)

Low-Pressure Performance of a Tubular Combustor With Gaseous Hydrogen

Memorandum presenting an investigation to determine the combustion performance characteristics of gaseous hydrogen fuel in a single tubular turbojet combustor. The combustor was operated over a range of inlet-air pressures from 3.3 to 14.3 inches of mercury absolute. Results regarding stability limits and combustion efficiency are provided.
Date: May 9, 1955
Creator: Jonash, Edmund R.; Smith, Arthur L. & Hlavin, Vincent F.
System: The UNT Digital Library
Line Broadening by Electrons : the Validity of Simple Theories (open access)

Line Broadening by Electrons : the Validity of Simple Theories

A comparison of the simple impact theories of line broadening by electrons with the detailed computations of Kivel, Bloom, and Margenau.
Date: May 9, 1955
Creator: Meyerott, Roland Edward & Margenau, Henry, 1901-1997.
System: The UNT Digital Library