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Aircraft Design with Electric Subsystems by 김영민 is a document available to read on EtoBox.
The paper discusses the challenges of integrating More Electric subsystem architectures in the early design stages of aircraft due to the lack of historical data and numerous architecture possibilities. It presents the Integrated Subsystem Sizing and Architecture Assessment Capability (ISSAAC), which allows for simultaneous aircraft and subsystem resizing to evaluate performance impacts. The study investigates various subsystem architectures for different aircraft sizes and performs sensitivity analysis on
- Author
- 김영민
- Language
- EN