The development of new supersonic passenger airplanes (SPA) requires the development of modern environmental control systems for them (ECS). The goal of this paper is to form a possible appearance of the ECS for the modern SPA. In order to achieve this goal, a number of tasks were accomplished: thermal and humidity calculations of the ECS characteristics were carried out in four flight modes, the ECS effectiveness was evaluated, the design of the proposed ECS scheme was analyzed, the influence of the flight mode on the operation of the ECS was evaluated, graphs of dependences of the ECS main efficiency indicators in supersonic flight mode were constructed.
Study of the Environmental Control System of a Supersonic Passenger Aircraft
2024-02-29
361426 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Supersonic passenger-carrying aircraft
Engineering Index Backfile | 1957
|Supersonic Passenger Aircraft: Concorde
Online Contents | 2013
Supersonic Passenger Aircraft part IV
Online Contents | 2014
Fuel for Supersonic Passenger Aircraft
NTIS | 1974
|Advanced Supersonic Passenger Aircraft Cockpit Technologies
Springer Verlag | 2023
|