Now showing items 1-6 of 6
Investigation of Poststall Pitch Oscillations of an Aircraft Wind-Tunnel Model
(American Institute of Aeronautics and Astronautics, AIAA, 2013-08)
A five-degree-of-freedom dynamic wind-tunnel rig is used in the observation of large-amplitude, stall-related and self-sustaining, pitch oscillations of a model aircraft. These oscillations are investigated on the dynamic ...
Aerodynamic model development and simulation of airliner spin for upset recovery
(EDP Sciences, 2013-06)
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of attack, sideslip and angular rate based on experimental data obtained in wind tunnels using static, forced oscillations ...
A new immersed boundary method for compressible Navier-Stokes equations.
(Taylor and Francis, 2013)
Synthetic Aerodynamics Modeling for Pilot Training in the Extended Flight Envelope
(Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2013), 2013-11-21)
Flight at high angles of attack is associated with a variety of types of aircraft departure and post stall behaviour. Every aircraft will exhibit specific set of flight characteristics in extended flight envelope. This ...
Adaptive runge-kutta discontinuous galerkin method for complex geometry problems on cartesian grid
A Cartesian grid method using immersed boundary technique to simulate the impact of body in fluid has become an important research topic in computational fluid dynamics because of its simplification, automation of grid ...