Scholarlink

Abstract <p>A numerical study of the flow aerodynamics of a cascade-type thrust reverser located in the outer contour of a turbofan engine carried out at the switch-on stage during the flap repositioning. The integral aerodynamic characteristics of the thrust reverser are determined in the modes during the transition from the forward to reverse thrust. The verification of the numerical model is carried out on the basis of experimental study results.</p>

错误：搜索内容不能为空，请输入英文关键词
错误：关键词超出字数限制，请精简
高级检索

Aerodynamics of the Thrust Reverser of a Turbofan Engine at the Switch-on Stage

  • 期刊论文

  • 发表日期：

    2025年9月1日

查看全文
  • V. L. Varsegov,
  • L. A. Saukhin

摘要

Abstract

A numerical study of the flow aerodynamics of a cascade-type thrust reverser located in the outer contour of a turbofan engine carried out at the switch-on stage during the flap repositioning. The integral aerodynamic characteristics of the thrust reverser are determined in the modes during the transition from the forward to reverse thrust. The verification of the numerical model is carried out on the basis of experimental study results.