6.7
Further ruminations on predicting icing severity
Obviously, a small single-engine airplane does not respond to an icing environment the same way a multi-engine jet does; there are disparities in capabilities of the aircraft that are not well-captured by the general severity descriptions these products provide. The ideal is an aircraft-specific severity index. This requires information for all three components of the problem: detailed size distributions of supercooled water drops (and perhaps ice crystals); full knowledge of the accretion physics and characteristics of the complete aircraft under all flight configurations; and an understanding of the response of that aircraft to the accreted ice. The current level of development , on the part of all three aspects, is a long way from that required to solve this problem. The problem and approaches to solutions will be discussed briefly.