REVIEW OF RECENT RESEARCH ON INTERIOR NOISE OF PROPELLER AIRCRAFT

被引：10

作者：

MIXSON, JS

POWELL, CA

机构：

[1] NASA, Langley Research Cent,, Hampton, VA, USA, NASA, Langley Research Cent, Hampton, VA, USA

来源：

JOURNAL OF AIRCRAFT | 1985年 / 22卷 / 11期

关键词：

D O I：

10.2514/3.45229

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

187

引用

页码：931 / 949

页数：19

共 187 条

[1] SINGLE-WALL AND DOUBLE-WALL CYLINDER NOISE-REDUCTION [J].

BALENA, FJ ;

PRYDZ, RA ;

REVELL, JD .

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[2] NOISE TRANSMISSION AND CONTROL FOR A LIGHT TWIN-ENGINE AIRCRAFT [J].

BARTON, CK ;

MIXSON, JS .

JOURNAL OF AIRCRAFT, 1981, 18 (07) :570-575

[3] CHARACTERISTICS OF PROPELLER NOISE ON AN AIRCRAFT FUSELAGE [J].

BARTON, CK ;

MIXSON, JS .

JOURNAL OF AIRCRAFT, 1981, 18 (03) :200-205

[4]

BARTON CK, 1978, NASA TP, V1321

[5]

BASSETT PR, 1934, T ASME FEB, P49

[6]

Beranek L. L., 1971, NOISE VIBRATION CONT

[7] SOUND TRANSMISSION THROUGH MULTIPLE STRUCTURES CONTAINING FLEXIBLE BLANKETS [J].

BERANEK, LL ;

WORK, GA .

JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1949, 21 (04) :419-428

[8] ACOUSTICAL PROPERTIES OF HOMOGENEOUS, ISOTROPIC RIGID TILES AND FLEXIBLE BLANKETS [J].

BERANEK, LL .

JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1947, 19 (04) :556-568

[9]

BEYER TB, 1984, AIAA842331 PAP

[10] INTERIOR NOISE RADIATED BY AN AIRPLANE FUSELAGE SUBJECTED TO TURBULENT BOUNDARY LAYER EXCITATION AND EVALUATION OF NOISE REDUCTION TREATMENTS [J].

BHAT, WV ;

WILBY, JF .

JOURNAL OF SOUND AND VIBRATION, 1971, 18 (04) :449-&

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