EXPERIMENTAL AND THEORETICAL STUDY OF FLOW OVER FINITE-WIDTH WEDGE AT SLIP ANGLES.

被引：0

作者：

Duganov, V.V.

Ivanov, O.K.

机构：

来源：

Soviet Aeronautics (English translation of Izvestiya VUZ, Aviatsionnaya Tekhnika) | 1984年 / 27卷 / 04期

关键词：

AERODYNAMICS; -; Supersonic;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Wedge-shaped bodies are used as the compression surfaces of two-dimensional supersonic air intakes. The finite width of the wedges leads to flow 'spreading', which causes reduction of the discharge coefficient. On the other hand, the flow near the side surfaces of such wedges is very nonuniform and it is necessary to consider its influence on the flight vehicle characteristics. This article presents a clarification of the structure of the three-dimensional flow.

引用

页码：126 / 129