Application of the “actuator disk” boundary condition to calculation of a non-uniform flow in the air intake of modern turbofan engines
Published: 15.08.2019
Authors: Nguyen V.H.
Published in issue: #8(92)/2019
DOI: 10.18698/2308-6033-2019-8-1909
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts