Propulsion and Power Plants
Аuthors
Abstract
A comparative effectiveness analysis is carried out for two gas-dynamic turbo-jet schemes namely for double-chamber turbo-jet schemes namely for double-chamber turbo-jet and for bypass reheated turbo-jet. The analysis is performed for a multiple-mode supersonic aircraft case.
mai.ru — informational site of MAI Copyright © 1994-2024 by MAI |