Experimental and Numerical Research of Lift Force Produced by Coanda Effect

被引：2

作者：

Constantinescu, S. G. ^{[1
]}

Niculescu, M. L. ^{[2
]}

机构：

[1] Dunarea de Jos Univ Galati, 47 Str Domneasca, Galati 800008, Romania

[2] INCAS, Natl Inst Aerosp Res, Bucharest 061126, Romania

来源：

11TH INTERNATIONAL CONFERENCE OF NUMERICAL ANALYSIS AND APPLIED MATHEMATICS 2013, PTS 1 AND 2 (ICNAAM 2013) | 2013年 / 1558卷

关键词：

Coanda effect; lift force; drone;

D O I：

10.1063/1.4825443

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

The paper presents research results of aerodynamics of Coanda airfoil, that is a key element of drones with jet propulsion. The Coanda propulsion allows drones to monitor quickly the large areas in emergencies: forest fires, earthquakes, meteor attacks and so on. The aim of this work consists in establishment of geometric and aerodynamic parameters at which, the lift force produced by Coanda airfoil is maximal.

引用

页码：152 / 155

页数：4