INFLUENCES OF WIND-TUNNEL PARAMETERS ON AIRFOIL CHARACTERISTICS AT HIGH SUBSONIC SPEEDS

被引：0
|
作者：
SCHEITLE, H [1 ]
WAGNER, S [1 ]
机构：
[1] UNIV MUNICH,INST LUFTFAHRTTECH & LEICHTBAU,W-8014 MUNICH,GERMANY
来源：
EXPERIMENTS IN FLUIDS | 1991年 / 12卷 / 1-2期
关键词：
D O I：
暂无
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The influences of several wind tunnel parameters on airfoil characteristics are experimentally investigated in a transonic wind tunnel. Quantified as Mach number errors they show decisive effects and confirm that they have to be taken into consideration in a valuation of test results. Differences in data gained in measurements of several wind tunnels can be partly explained thereby.
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页码：90 / 96
页数：7
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