A design approach for a model-scale VTOL powered by two pivoting kerosine turbines

At the Institute of Air Transportation Systems, an innovative vertical take-off and landing (VTOL) model is being developed as a test vehicle to stimulate future research on combined highly automated flying and ground systems. The aircraft, primarily powered by two pivoting kerosene turbines, will serve as a multi-role transport aircraft for different mission scenarios, resulting in different payloads. Intended missions include surveillance in disaster scenario, ground and airborne vehicle jettison during landing or in-flight, and flight algorithm testing. The research question is how the design can be achieved and what design methodologies are appropriate. This paper describes the design methodology for the aircraft design process according to the given requirements and presents two of the main aircraft concepts under consideration. It also details the key steps in the process, such as iterating and alternating designs. The aim of the paper is to provide a design methodology that motivates disruptive variation for more efficient design evolution.

Subjects

aircraft design

design methodology

design philosophy

UAV design

VTOL

DDC Class

629.13: Aviation Engineering

Options

A design approach for a model-scale VTOL powered by two pivoting kerosine turbines