NOISE DUE TO TURBULENT-FLOW PAST A TRAILING EDGE

[11] ECKERT ER, 1959, HEAT MASS TRANSFER, P144

[12] EXPERIMENTAL EVALUATION OF THEORIES FOR TRAILING EDGE AND INCIDENCE FLUCTUATION NOISE [J]. AIAA JOURNAL, 1975, 13 (11) : 1472 - 1477

[13] SIMILARITY RULES FOR THIN AEROFOILS IN NON-STATIONARY SUBSONIC FLOWS [J]. JOURNAL OF FLUID MECHANICS, 1970, 43 : 753 - &

[14] HAYDEN RE, 1972, CR2126 NASA

[15] Hinze J.O, 1975, TURBULENCE

[16] LIFT ON A WING IN A TURBULENT-FLOW [J]. AERONAUTICAL QUARTERLY, 1973, 24 (AUG): : 155 - 166

[17] Jones D., 1972, J I MATH APPL, V9, P114

[18] KEMP NH, TO BE PUBLISHED

[19] LANDAHL M, 1961, UNSTEADY TRANSONIC F, P27

[20] EXTENSION OF THE STATISTICAL APPROACH TO BUFFETING AND GUST RESPONSE OF WINGS OF FINITE SPAN [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (03): : 197 - 200

[11] ECKERT ER, 1959, HEAT MASS TRANSFER, P144

[12] EXPERIMENTAL EVALUATION OF THEORIES FOR TRAILING EDGE AND INCIDENCE FLUCTUATION NOISE [J]. AIAA JOURNAL, 1975, 13 (11) : 1472 - 1477

[13] SIMILARITY RULES FOR THIN AEROFOILS IN NON-STATIONARY SUBSONIC FLOWS [J]. JOURNAL OF FLUID MECHANICS, 1970, 43 : 753 - &

[14] HAYDEN RE, 1972, CR2126 NASA

[15] Hinze J.O, 1975, TURBULENCE

[16] LIFT ON A WING IN A TURBULENT-FLOW [J]. AERONAUTICAL QUARTERLY, 1973, 24 (AUG): : 155 - 166

[17] Jones D., 1972, J I MATH APPL, V9, P114

[18] KEMP NH, TO BE PUBLISHED

[19] LANDAHL M, 1961, UNSTEADY TRANSONIC F, P27

[20] EXTENSION OF THE STATISTICAL APPROACH TO BUFFETING AND GUST RESPONSE OF WINGS OF FINITE SPAN [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (03): : 197 - 200