FIELD: aviation and ecology; environmental control.
SUBSTANCE: proposed method consists in measurement of altitude H in cruising flights, pressure P, temperature tHB, partial pressure steam contained in atmospheric air eHB, turbine exhaust gas temperature tt and rotational speed of engine, calculation of temperature gradient of moisture mixed with exhaust jet B0. Besides that, magnitude of quantitative parameter of steam super-saturation in mixed exhaust jet of engine is calculated by definite formula.
EFFECT: possibility of normalizing of quantitative characteristics of condensation trails depending on their effect on radiation balance of atmosphere and ground surface for reduction of content of carbon dioxide in exhaust jet of aircraft engine.
1 dwg
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Authors
Dates
2007-12-10—Published
2006-01-11—Filed