THEORETICAL INVESTIGATION OF LAMINAR WAKES BEHIND AIRFOILS AND RESULTING NOISE PATTERN

[1] [Anonymous], 1974, J AIRCRAFT

[2] VORTEX SHEDDING FROM THIN FLAT PLATES PARALLEL TO THE FREE STREAM [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (04): : 340 - 341

[3] Durand W.F., 1935, AERODYNAMIC THEORY, VII

[4] H. Schlichting, 1968, BOUNDARY LAYER THEOR

[5] Karman TV, 1938, J AERONAUTICAL SCIEN, V5, P379

[6] Morse P. M., 1987, THEORETICAL ACOUSTIC

[7] Paterson R.W., 1973, J AIRCRAFT, V10, P296, DOI [10.2514/3.60229, DOI 10.2514/3.60229]

[8] Sallet DW, 1973, J HYDRONAUT, DOI 10.2514/3.62951

[9] TOROBIN LB, 1959, CAN J CHEM ENG, V37, P167, DOI DOI 10.1002/CJCE.5450370501

[10] TYLER E, 1931, PHILOSOPHICAL MAGAZI, V2, P7

[1] [Anonymous], 1974, J AIRCRAFT

[2] VORTEX SHEDDING FROM THIN FLAT PLATES PARALLEL TO THE FREE STREAM [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (04): : 340 - 341

[3] Durand W.F., 1935, AERODYNAMIC THEORY, VII

[4] H. Schlichting, 1968, BOUNDARY LAYER THEOR

[5] Karman TV, 1938, J AERONAUTICAL SCIEN, V5, P379

[6] Morse P. M., 1987, THEORETICAL ACOUSTIC

[7] Paterson R.W., 1973, J AIRCRAFT, V10, P296, DOI [10.2514/3.60229, DOI 10.2514/3.60229]

[8] Sallet DW, 1973, J HYDRONAUT, DOI 10.2514/3.62951

[9] TOROBIN LB, 1959, CAN J CHEM ENG, V37, P167, DOI DOI 10.1002/CJCE.5450370501

[10] TYLER E, 1931, PHILOSOPHICAL MAGAZI, V2, P7