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About Eects of Aircraft Integration On Compact Nacelle Aerodynamics
This document summarizes a study on the effects of aircraft integration on compact nacelle aerodynamics. The study uses computational fluid dynamics and multi-objective optimization techniques to design compact nacelle configurations for future high-bypass ratio aircraft engines. The optimized nacelle designs are then installed on a commercial aircraft and evaluated at different positions. For a close-coupled installation position expected for future engines, the optimized compact nacelle design is shown to increase the net vehicle force by 0.44% compared to a conventional nacelle design.
Detailed Information
| Author: | ['Hao Liu'] |
|---|---|
| Publication Year: | 2021 |
| Pages: | 35 |
| Language: | English |
| Format: | |
| Price: | FREE |
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