Natural Icing of an Axial-Flow Turbojet Engine in Flight for a Single Icing Condition
Description:
Memorandum presenting an investigation in natural icing conditions to determine the effect of ice formations on the performance of an axial-flow turbojet engine. A description of the change over time in tail-pipe temperature, engine jet thrust, fuel flow, ice collection, and acceleration qualities are provided.
Date:
August 12, 1948
Creator:
Acker, Loren W.
Partner:
UNT Libraries Government Documents Department