PROPELLER AIRCRAFT INTERIOR NOISE MODEL .1. ANALYTICAL MODEL

被引：16

作者：

POPE, LD ^{[1
]}

WILBY, EG ^{[1
]}

WILBY, JF ^{[1
]}

机构：

[1] BBN LABS,CANOGA PK,CA 91305

来源：

JOURNAL OF SOUND AND VIBRATION | 1987年 / 118卷 / 03期

关键词：

D O I：

10.1016/0022-460X(87)90364-6

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

引用

页码：449 / 467

页数：19

共 12 条

[1]

MAGLIOZZI B, 1980, J AIRCRAFT, V19, P104

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PETERSON, MR ;

BOYD, DE .

JOURNAL OF SOUND AND VIBRATION, 1978, 60 (01) :45-62

[3]

PETERSON MR, 1973, THESIS OKLAHOMA STAT

[4] BAND-LIMITED POWER FLOW INTO ENCLOSURES [J].

POPE, LD ;

WILBY, JF .

JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1977, 62 (04) :906-911

[5] BAND-LIMITED POWER FLOW INTO ENCLOSURES .2. [J].

POPE, LD ;

WILBY, JF .

JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1980, 67 (03) :823-826

[6] DEVELOPMENT AND VALIDATION OF PRELIMINARY ANALYTICAL MODELS FOR AIRCRAFT INTERIOR NOISE PREDICTION [J].

POPE, LD ;

RENNISON, DC ;

WILLIS, CM ;

MAYES, WH .

JOURNAL OF SOUND AND VIBRATION, 1982, 82 (04) :541-575

[7] AIRCRAFT INTERIOR NOISE MODELS - SIDEWALL TRIM, STIFFENED STRUCTURES, AND CABIN ACOUSTICS WITH FLOOR PARTITION [J].

POPE, LD ;

WILBY, EG ;

WILLIS, CM ;

MAYES, WH .

JOURNAL OF SOUND AND VIBRATION, 1983, 89 (03) :371-417

[8]

POPE LD, 1984, NASA CR172428

[9]

POPE LD, 1984, NASA CR3813

[10]

WILBY EG, 1984, NASA CR172425

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