Tez Dosyaları 14
Cessna 172 hibrit-elektrik retrofit entegrasyonu ve performans modellemesi
Unsteady aerodynamics of cambered airfoils at low Reynolds number
Automated hybrid-electric propulsion architecturemodeling for conceptual aircraft design: A novel approachto integrating system architecting in MDO
Implementation of an actuator disc model using blade element theory for propellers into SU2 software
Development of Unsteady Models for Flapping Wings’ Controller Design Approach
UNSTEADY AERODYNAMIC CHARACTERISTICS OF SYMMETRIC AIRFOIL AT LOW REYNOLDS NUMBERS
2D AND 3D UNSTEADY AERODYNAMIC ANALYSIS OF A VERY LIGHTAIRCRAFT'S WING
, Numerical and Experimental Investigation of Pitching/Plunging Airfoils in Hover
MODEL BASED PRELIMINARY DESIGN AND OPTIMIZATION OF AIRCRAFTS
Aerodynamic analysis of flapping wing actuated with pzt material including aeroelastic deformation
Investigation of the flexible missile fins under aerothermal loading
Modeling of the hawkmoth wing and its implementation in a four-bar flapping wing mechanism
Unsteady aerodynamics of plunging and stationary symmetric airfoils at low Reynolds numbers
Aerodynamic and inertial characterization of a generic flapping wing mechanism