Study on Proprotor Airfoil Optimization for Improving Aerodynamic Performance of Tiltrotor Aircraft, Part Ⅱ: Evaluation of Proprotor Performance
Year: 2025
Type: article
Abstract: 틸트로터형 항공기(Tiltrotor Aircraft)는 고정익기(Fixed Wing Aircraft)의 동체 형 상을 가지면서 비행 모드에 따라 회전축의 각도(Shaft Angle)를 조절할 수 있는 프롭 로터
Authors: D.H. Kang, N.E. Park, J.D. Cho, S.H. Park
Institutions: Konkuk University, Korea Aerospace Industries (South Korea)
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: hybrid
OpenAlex ID: W4412101263