Aeroelastic stability of full-span tiltrotor aircraft model in forward flight
نویسندگان
چکیده
منابع مشابه
Aeroelastic Tailoring of a Civil Tiltrotor Configuration
Progress in establishing an analysis package and design/optimization framework for preliminary design of a civil tiltrotor aircraft is reported. Updates to the sizing/performance program VASCOMP and Equivalent LAminated Plate Solution ELAPS are described. Correlation of this updated ELAPS (now including shear panels) and a state-space unsteady aerodynamic analysis, PWAKE, with reference results...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2017
ISSN: 1000-9361
DOI: 10.1016/j.cja.2017.09.007