DATA exist now for the design of heated wings on a fundamental wet-air basis. The design method takes into consideration three factors: All of the water intercepted by a wing which is to be heated only in the leading-edge region must be dispersed by evaporation. The design method provides for determining the heat required and the extent of heated area needed to evaporate the intercepted water.
Calculation of Heat Required for WING THERMAL ICE PREVENTION in Specified Icing Conditions
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
1948-01-01
Aufsatz (Konferenz)
Englisch
Calculation of heat required for wing thermal ice prevention in specified icing conditions
Engineering Index Backfile | 1947
|Engineering Index Backfile | 1946
|Europäisches Patentamt | 2021
|Online Contents | 1994