DETERMINATION OF REVERSER TURNING CASCADE IMPINGEMENT ANGLES.

被引：0

作者：

Maklakov, D.V.

Rogalev, V.V.

机构：

来源：

Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika) | 1984年 / 27卷 / 03期

关键词：

FLOW OF FLUIDS - Cascades - GAS TURBINES;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

We examine plane steady-state potential discharge of ideal incompressible fluid from a channel having a blocking flap EF and a turning cascade. The channel simulates the meridional section of a reverser located in the outer duct of a bypass turbojet engine (BTJE).

引用

页码：125 / 127