A THEORETICAL STUDY OF HELICOPTER ROTOR NOISE

被引:89
作者
LOWSON, MV
OLLERHEA.JB
机构
关键词
D O I
10.1016/0022-460X(69)90028-5
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
引用
收藏
页码:197 / &
相关论文
共 30 条
[1]  
ARNOLD I, 1961, TR221 GEN APPL SCIEN
[2]  
BURPO FB, 1962, TCREC6242 US ARM TRA
[3]  
COX CR, 1962, TCREC6273 US ARM TRA
[4]  
Davidson I.M., 1965, J R AERONAUT SOC, V69, P653
[5]  
GARRICK IE, 1954, NACA1198 REP NAT ADV
[6]  
GUTIN L, 1936, PHYS Z SOWJETUNION A, V1, P57
[7]   NOISE CHARACTERISTICS OF HELICOPTER ROTORS AT TIP SPEEDS UP TO 900-FEET-PER-SECOND [J].
HUBBARD, HH ;
MAGLIERI, DJ .
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1960, 32 (09) :1105-1107
[8]  
LEVERTON JW, 1966, J SOUND VIB, V4, P345
[9]  
LEVI H, 1928, P R SOC A, V120, P670
[10]   ON SOUND GENERATED AERODYNAMICALLY .1. GENERAL THEORY [J].
LIGHTHILL, MJ .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1952, 211 (1107) :564-587