THEORETICAL TREATMENT OF GUST SIMULATION IN THE WIND-TUNNEL

被引:0
作者
LASCHKA, B
WEGNER, W
机构
[1] Technische Univ Braunschweig, West Ger, Technische Univ Braunschweig, West Ger
来源
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 1986年 / 10卷 / 03期
关键词
AERODYNAMICS - Lift - AIRCRAFT - Stability - FLOW OF FLUIDS - Unsteady Flow;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
During the past years gust generators consisting of a system of oscillating lifting surfaces have been or are being prepared for use in wind tunnels. The corresponding gust field can be assessed by applying unsteady wing theory. In the present report, the basic relationships for the calculation of the flow parameters of coupled lifting surfaces in incompressible flow are presented. Results for both aerodynamic forces and the flow field are given.
引用
收藏
页码:168 / 173
页数:6
相关论文
共 6 条
[1]  
FREYMANN R, 1985, DFVLRFB8504
[2]  
KRAG B, 1982, DFVLRFB8226
[3]  
KRAG B, 1985, AGARD FDP FMP S GOTT
[4]  
LASCHKA B, 1970, Z FLUGWISSENSCH, V18, P359
[5]  
Laschka B., 1963, Z FLUGWISSENSCHAFTEN, V11, P265
[6]  
LASCHKA B, 1977, NEUE ERGEBNISSE EBEN