VORTEX INDUCED HELICOPTER BLADE LOADS AND NOISE

被引：4

作者：

FILOTAS, LT ^{[1
]}

机构：

[1] MINIST TRANSPORT,CIVIL AVIATION BRANCH,OTTAWA K1A ON8,ONTARIO,CANADA

来源：

关键词：

D O I：

10.1016/S0022-460X(73)80353-0

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

引用

页码：387 / 398

页数：12

共 14 条

CLARK, PFJ ;

RIBNER, HS .

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[3]

Filotas L. T., 1971, J AIRCRAFT, V8, P395, DOI 10.2514/3.44277

[4]

FILOTAS LT, 1969, UTIAS139 U TOR I AER

[5]

GIESING JP, 1969, 5368 DOUGL AIRCR CO

GRAHAM, JMR .

[7]

HORLOCK JH, 1968, J BASIC ENGINEERIN D, V90, P495

[8] LIFTING-SURFACE SOLUTION FOR VORTEX-INDUCED AIRLOADS [J].

JOHNSON, W .

[9]

LEVERTON JW, 1972, CR1983 NASA

[10]

LEVERTON JW, 1968, CR1221 NASA