IMPORTANCE OF AN ACCURATE PREDICTION OF SHOCK CURVATURE FOR HIGH-SPEED ROTOR NOISE

被引:2
作者
PRIEUR, J
机构
[1] Aeroacoustics Engineer, Onera, France
关键词
Rotors;
D O I
10.4050/JAHS.37.82
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
High-speed rotor noise predictions are performed by means of the ONERA quadrupolar code in the frequency domain. Calculations start from different shock geometries. Results are compared to US Army experiments and discussed. The noise calculation appears to be extremely dependent on the curvature of the shock.
引用
收藏
页码:82 / 85
页数:4
相关论文
共 10 条
[1]  
FARASSAT F, 1990, 46TH AM HEL SOC ANN
[2]  
FARASSAT F, 1988, J AM HEL SOC, V33
[3]  
HANSON DB, 1979, J SOUND VIB, V62
[4]  
ISOM MP, 1987, 11TH AER C SUNN
[5]  
PRIEUR J, 1988, AIAA J, V26
[6]  
PRIEUR J, 1986, 11TH AER C SEATTL
[7]  
PURCELL TW, 1988, 14 EUR ROT FOR MIL
[8]  
SCHMITZ FH, 1980, 6TH EUR ROT POW LIFT
[9]  
SCHMITZ FH, 1981, VERTICA, V5
[10]  
WELLS V, 1989, 12TH AER C SAN ANT