SOME FEATURES OF BYPASS ENGINE OPERATION PROCESS WITH SEPARATE EXHAUST NOZZLES

In the article some equations are derived to establish the relationships between the thermodynamic cycle parameters applying to bypass engines with separate exhaust nozzles. Necessary calculations are made and the main dependences are analyzed. Some of them have not been analyzed in the famous artic...

Full description

Bibliographic Details
Main Authors: V. V. Medvedev, V. T. Shulekin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/326