Development of an aircraft worst case flutter prediction with Mach variation using robust stability analysis | Taehyoun Kim 교수 연구실 |

|Taehyoun Kim 교수 연구실

홈

연구 영역

기본 정보

논문·특허

구성원

Article|

인용수 8

·2009

Development of an aircraft worst case flutter prediction with Mach variation using robust stability analysis

Chan Hoon Chung, Sang Joon Shin, Taehyoun Kim

Journal of Mechanical Science and Technology

키워드

FlutterAerodynamicsMach numberAeroelasticityAerospace engineeringAerodynamic forceDynamic pressureCompressibilityLongitudinal static stabilityControl theory (sociology)EngineeringStructural engineeringMechanicsComputer sciencePhysics

타입

Article

IF / 인용수

- / 8

원문

https://doi.org/10.1007/s12206-009-0506-1

게재 연도

2009