Description: Memorandum presenting an investigation to determine the energy transfer by thermal radiation from the flame of a single tubular turbojet-engine combustor to the combustor liner. The effects of variations in combustor inlet-air pressure, fuel-air ratio, and air mass flow on the transfer of radiant energy were studied.
Date: August 19, 1952
Creator: Topper, Leonard
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department