Aerodynamic Design and Experimental Investigation of Short Nacelles for Future Turbofan Engines
Licentiate thesis, 2020
This thesis presents a newly developed methodology for multi-point design of ultra-short nacelles. An integrated aerodynamic framework, based on parametric geometry generation and computational fluid dynamics (CFD) flow solutions was built and used for designing several ultra-short nacelle shapes and to evaluate their aerodynamic performance. The main design parameters and their influence in the flow field were investigated for the most critical operating conditions among the flight mission, such as cruise, high angle-of-attack (AoA) and crosswind. The aerodynamic performance of the designed nacelles was evaluated through a thrust and drag bookkeeping approach, and also by means of the distortion levels at the fan face.
Furthermore, this work summarizes the main results obtained in an experimental aerodynamic investigation of a powered turbofan nacelle, conducted at the Chalmers low-speed wind tunnel. The impact of the engine angle-of-attack and the mass flow ratio (MFR) on the nacellle aerodynamic performance was investigated.
ultra-high-bypass turbofan
Computational Fluid Dynamics
powered nacelle.
Ultra-short nacelles
experimental
thrust-and-drag bookkeeping
Author
Vinícius Tavares Silva
Chalmers, Mechanics and Maritime Sciences (M2), Fluid Dynamics
Silva, V.T., Lundbladh, A., Xisto, C., Petit, O. Multi-point Aerodynamic Design of Ultra-short Nacelles for Ultra-high Bypass Turbofan EnginesMulti-point Aerodynamic Design of Ultra-short Nacelles for Ultra-high Bypass Turbofan Engines
Driving Forces
Sustainable development
Areas of Advance
Transport
Subject Categories
Aerospace Engineering
Fluid Mechanics and Acoustics
Infrastructure
Chalmers Laboratory of Fluids and Thermal Sciences
Thesis for the degree of Licentiate – Department of Mechanics and Maritime Sciences
Publisher
Chalmers