UNSTEADY AIRFOILS

[21] FUNG YC, 1969, THEORY AEROELASTICIT, P401

[22] GARNER HC, 1975, RAE TR74181

[23] GARRICK IE, 1981, AIAA810591CP PAP

[24] Giesing J. P., 1968, J AIRCRAFT, V5, P135, DOI DOI 10.2514/3.43920

[25] HAMAD G, 1980, AIAA800151 PAP

[26] UNSTEADY NEWTON-BUSEMANN FLOW THEORY .1. AIRFOILS [J]. AIAA JOURNAL, 1981, 19 (03) : 311 - 318

[27] APPROXIMATE UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW [J]. AIAA JOURNAL, 1976, 14 (08) : 1083 - 1089

[28] KUSSNER H. G., 1960, AGARD MANUAL AEROE 2

[29] KWAK D, 1981, AIAA J

[30] LAMBOURNE NC, 1968, AGARD MANUAL AEROE 5, pCH5

[21] FUNG YC, 1969, THEORY AEROELASTICIT, P401

[22] GARNER HC, 1975, RAE TR74181

[23] GARRICK IE, 1981, AIAA810591CP PAP

[24] Giesing J. P., 1968, J AIRCRAFT, V5, P135, DOI DOI 10.2514/3.43920

[25] HAMAD G, 1980, AIAA800151 PAP

[26] UNSTEADY NEWTON-BUSEMANN FLOW THEORY .1. AIRFOILS [J]. AIAA JOURNAL, 1981, 19 (03) : 311 - 318

[27] APPROXIMATE UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW [J]. AIAA JOURNAL, 1976, 14 (08) : 1083 - 1089

[28] KUSSNER H. G., 1960, AGARD MANUAL AEROE 2

[29] KWAK D, 1981, AIAA J

[30] LAMBOURNE NC, 1968, AGARD MANUAL AEROE 5, pCH5