FLIGHT TEST MEASUREMENT OF EXTERIOR TURBULENT BOUNDARY LAYER PRESSURE FLUCTUATIONS ON BOEING-MODEL-737 AIRPLANE

被引：46

作者：

BHAT, WV

机构：

来源：

关键词：

D O I：

10.1016/0022-460X(71)90574-8

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

引用

页码：439 / &

共 19 条

[1] EFFECTS OF ROUGHNESS ON MEASURED WALL-PRESSURE FLUCTUATIONS BENEATH A TURBULENT BOUNDARY LAYER
AUPPERLE, FA
LAMBERT, RF
[J]. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1970, 47 (1P2) : 359 - &
[2] BELCHER PM, 1965, 5 P INT C ACOUST LIE
[3] BLACK TJ, 1968, CR888 NASA
[4] BLAKE WK, 1969, 702081 MASS I TECHN
[5] BULL MK, 1963, AASU234 U SOUTH
[6] CHYU WJ, 1968, 6 AIAA AER SCIENC M
[7] RESOLUTION OF PRESSURE IN TURBULENCE
CORCOS, GM
[J]. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1963, 35 (02) : 192 - &
[8] CORCOS GM, 1958, SM19570 DOUGL AIRCR
[9] RESPONSE OF A SUPERSONIC TRANSPORT FUSELAGE TO BOUNDARY LAYER AND TO REVERBERANT NOISE
CROCKER, MJ
[J]. JOURNAL OF SOUND AND VIBRATION, 1969, 9 (01) : 6 - &
[10] Gebhardt GT, 1965, J AIRCRAFT, V2, P272, DOI 10.2514/3.43652