THEROETICAL CONSIDERATIONS OF PANEL FLUTTER AT HIGH SUPERSONIC MACH NUMBERS

[1] PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12): : 1109 - 1118

[2] BOHON HL, 1964, J AIRCRAFT, V1, P280, DOI DOI 10.2514/3.43594

[3] Bolotin V.V., 1963, NONCONSERVATIVE PROB

[4] FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON 3-DIMENSIONAL SUPERSONIC POTENTIAL FLOW [J]. AIAA JOURNAL, 1963, 1 (08) : 1795 - 1801

[5] DOWELL E, 1964, 641723 AIR FORC OFF

[6] THEORETICAL AND EXPERIMENTAL PANEL FLUTTER STUDIES IN MACH NUMBER RANGE 1.0 TO 5.0 [J]. AIAA JOURNAL, 1965, 3 (12) : 2292 - &

[7] DOWELL EH, 1964, TR1122 MASS I TECHN

[8] PURE BENDING FLUTTER OF A SWEPT WING IN A HIGH-DENSITY LOW-SPEED FLOW [J]. AIAA JOURNAL, 1965, 3 (06) : 1126 - &

[9] DUGUNDJI J, 1965, TR1341 MASS I TECHN

[10] FRALICH RW, 1963, NASATND1615 LANGL RE

[1] PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12): : 1109 - 1118

[2] BOHON HL, 1964, J AIRCRAFT, V1, P280, DOI DOI 10.2514/3.43594

[3] Bolotin V.V., 1963, NONCONSERVATIVE PROB

[4] FLUTTER ANALYSIS OF FLAT RECTANGULAR PANELS BASED ON 3-DIMENSIONAL SUPERSONIC POTENTIAL FLOW [J]. AIAA JOURNAL, 1963, 1 (08) : 1795 - 1801

[5] DOWELL E, 1964, 641723 AIR FORC OFF

[6] THEORETICAL AND EXPERIMENTAL PANEL FLUTTER STUDIES IN MACH NUMBER RANGE 1.0 TO 5.0 [J]. AIAA JOURNAL, 1965, 3 (12) : 2292 - &

[7] DOWELL EH, 1964, TR1122 MASS I TECHN

[8] PURE BENDING FLUTTER OF A SWEPT WING IN A HIGH-DENSITY LOW-SPEED FLOW [J]. AIAA JOURNAL, 1965, 3 (06) : 1126 - &

[9] DUGUNDJI J, 1965, TR1341 MASS I TECHN

[10] FRALICH RW, 1963, NASATND1615 LANGL RE