DIGITAL COMPUTER SIMULATION OF THE AIR INTAKE LIP AND INLET GUIDE VANES GEOMETRY IN «COUNTER- ROTATING AIR BLADES - SUBSONIC INTAKE DUCT» SYSTEM OF THE TURBOPROP AIRCRAFT ENGINE ON ITS AERODYNAMIC CHARACTERISTICS

Autor: Komarov, V.V.

Publikováno v: Herald of Aeroenginebuilding; № 1 (2018): Herald of aeroenginebuilding
Вестник двигателестроения; № 1 (2018): Вестник двигателестроения
Вісник двигунобудування; № 1 (2018): Вісник двигунобудування

The purpose of the paper is to develop methodology for determining the parameters of the «counter- rotating air blades — subsonic intake duct» systems of a turboprop aircraft engine and develop recommendations on turboprop aircraft engine subsoni

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::2fe1ad2e0b104ea636c2005b75f34852
http://vd.zntu.edu.ua/article/view/150528