Computational study of the aircraft condensation trail formation
| Authors: Apraksin D.V., Voronich I.V. | Published: 21.08.2025 |
| Published in issue: #8(785)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: passenger aircraft, bypass turbofan engine, jet, condensation trails, cocurrent flow, water vapor emission |
The paper considers a problem in determining conditions for the aircraft condensation trail formation when mixing the bypass turbofan engine jet with a cocurrent flow (atmosphere). Approach to solving the problem is based on a numerical solution of the gas dynamics equations system (Reynolds equations) taking into account configuration of the bypass turbofan engine nozzle section. Computation uses the geometric and gas-dynamic parameters that affect the phenomena under consideration for several types of the bypass turbofan engines, and includes the bypass ratio, parameters of the internal and external flows, water vapor emission, etc. Study results are required to substantiate the criterion for formation of the aircraft stable condensation trails using the supersaturation degree of the water vapor in an engine jet. The paper analyzes examples of forming the aircraft condensation trails based on the known data from the flight experiments.
EDN: OKOHOG, https://elibrary/okohog
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