Study on Korean In-Flight Simulator Aircraft

Steady Aircraft Flight and Aircraft Performance

In-Trim Flight Investigations of a Conceptual Fluidic Thrust-Vectored Unmanned Tail-Sitter Aircraft

The feasibility of using a stand alone Fluidic Thrust-Vectoring (FTV) system for the purpose of longitudinal trim of an unmanned aerial vehicle is the focus of the research presented in this paper. Since the fluidic thrust vectoring requires high pressure secondary air to deflect the engine exhaust gases, this research also provides an analytical toolset for preliminary sizing of a suitable sec...

calculation of aircraft aerodynamic loads during operational flight

in this research, the calculation method of aerodynamic loads on an airplane in all flight situations is presented. in order to find an calculation equation for aerodynamic loads on an airplane in all flight conditions, the f-5 aircraft is selected as a prototype is divided into one hundred small parts longitudinally. therefore, the numerical solutions are taken place in different conditions of...

Vision-only Aircraft Flight Control

1 Graduate Research Assistant Email: [email protected] 2 Graduate Research Assistant Email: [email protected] 3 Lockheed Martin Assistant Professor of Avionics Integration Email: [email protected] Abstract Building aircraft with navigation and control systems that can complete flight tasks is complex, and often involves integrating information from multipl...

Aircraft Engine Performance Study Using Flight Data Recorder Archives

Aircraft emissions are a significant source of pollution and are closely related to engine fuel burn. The onboard Flight Data Recorder (FDR) is an accurate source of information as it logs operational aircraft data in situ. The main objective of this paper is the visualization and exploration of data from the FDR. The Airbus A330 223 is used to study the variation of normalized engine performan...