Searched for: subject%3A%22Pusher%255C%2Bpropeller%22
(1 - 4 of 4)
document
Garg, Sparsh (author)
It is the need of the hour to focus research and development towards curbing emissions due to the growing aviation industry. Employing boundary layer Ingesting(BLI) propellers for development of propulsive fuselage concept(PFC) aircraft while utilizing hydrogen as an alternative energy source, is the idea behind project APPU(Advanced Propulsion...
master thesis 2022
document
Mota Mera, Antonio (author)
The present work has placed particular importance on the spinner aerodynamic design in order to enhance the performance of a pusher propeller configuration. The research has been focused on the aerodynamic shaping of the spinner in order to provide a better understanding of the nacelle-blade-spinner interaction in cruise conditions. The set of...
master thesis 2020
document
Sinnige, T. (author), Ragni, D. (author), Malgoezar, A.M.N. (author), Eitelberg, G. (author), Veldhuis, L.L.M. (author)
Advanced propellers promise significant fuel-burn savings compared to turbofans. When installed on the fuselage in a pusher configuration, the propeller interacts with the wake of the supporting pylon. This paper presents an experimental analysis of the aerodynamic and aeroacoustic characteristics of this pylon–propeller interaction. An isolated...
journal article 2017
document
Van Arnhem, N. (author)
Boundary Layer Ingestion is an integrated propulsion concept in which a propulsor operates in boundary layer flow instead of the free streamflow with the goal to reduce the fuel flow for a given operating condition. The objective of this thesis is to obtain a better understanding of the power benefit of an installed pusher propeller at the aft...
master thesis 2015
Searched for: subject%3A%22Pusher%255C%2Bpropeller%22
(1 - 4 of 4)