NOISE GENERATED BY AIRFOIL PROFILES PLACED IN A UNIFORM LAMINAR-FLOW

[1] [Anonymous], 1974, J AIRCRAFT

[2] ARBEY H, 1981, THESIS U C BERNARD L

[3] LAMINAR BOUNDARY-LAYER INSTABILITY EXCITATION OF AN ACOUSTIC RESONANCE [J]. JOURNAL OF SOUND AND VIBRATION, 1975, 38 (03) : 387 - 402

[4] THEORETICAL INVESTIGATION OF LAMINAR WAKES BEHIND AIRFOILS AND RESULTING NOISE PATTERN [J]. JOURNAL OF SOUND AND VIBRATION, 1977, 50 (01) : 133 - 144

[5] GAUDRIOT L, 1982, REV ACOUST, V63, P208

[6] HENRY C, 1975, THESIS U C BERNARD L

[7] REVIEW OF THE THEORY OF TRAILING EDGE NOISE [J]. JOURNAL OF SOUND AND VIBRATION, 1978, 61 (03) : 437 - 465

[8] VORTEX SHEDDING NOISE OF LOW TIP SPEED, AXIAL-FLOW FANS [J]. JOURNAL OF SOUND AND VIBRATION, 1977, 53 (01) : 25 - 46

[9] COMPUTING METHOD FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYER WITH HEAT-TRANSFER [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1976, 19 (08) : 893 - 899

[10] Obremski H., 1969, PORTFOLIO STABILITY

[1] [Anonymous], 1974, J AIRCRAFT

[2] ARBEY H, 1981, THESIS U C BERNARD L

[3] LAMINAR BOUNDARY-LAYER INSTABILITY EXCITATION OF AN ACOUSTIC RESONANCE [J]. JOURNAL OF SOUND AND VIBRATION, 1975, 38 (03) : 387 - 402

[4] THEORETICAL INVESTIGATION OF LAMINAR WAKES BEHIND AIRFOILS AND RESULTING NOISE PATTERN [J]. JOURNAL OF SOUND AND VIBRATION, 1977, 50 (01) : 133 - 144

[5] GAUDRIOT L, 1982, REV ACOUST, V63, P208

[6] HENRY C, 1975, THESIS U C BERNARD L

[7] REVIEW OF THE THEORY OF TRAILING EDGE NOISE [J]. JOURNAL OF SOUND AND VIBRATION, 1978, 61 (03) : 437 - 465

[8] VORTEX SHEDDING NOISE OF LOW TIP SPEED, AXIAL-FLOW FANS [J]. JOURNAL OF SOUND AND VIBRATION, 1977, 53 (01) : 25 - 46

[9] COMPUTING METHOD FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYER WITH HEAT-TRANSFER [J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1976, 19 (08) : 893 - 899

[10] Obremski H., 1969, PORTFOLIO STABILITY