MEMORANDUM REPORT for the Air Technical Service Command, Army Air Forces LABORATORY INVESTIGATION OF ICING IN TEE CARBURETOR ADD SUPERCHARGER INLET ELBOW OF AN AIRCRAFT ENGINE Ⅱ - DETERMINATION OF THE LIMITING-ICING CONDITIONS

摘要

The carburetor and engine-stage supercharger assembly of a fighter aircraft were laboratory-tested to determine the Icing characteristics of the induction system under three simulated engine power conditions with varying carburetor-air temperature, relative humidity, simulated-rain injection, rain and fuel temperature, fuel-air ratio, and fuel of different distillation characteristics.