A UNIFIED SET OF SINGLE STEP ALGORITHMS .3. THE BETA-M METHOD, A GENERALIZATION OF THE NEWMARK SCHEME

[1] A ONE-STEP METHOD FOR DIRECT INTEGRATION OF STRUCTURAL DYNAMIC EQUATIONS [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1980, 15 (05) : 685 - 699

[2] Dahlquist GG, 1963, BIT, V3, P27, DOI [10.1007/BF01963532, DOI 10.1007/BF01963532]

[3] Henrici P, 1962, DISCRETE VARIABLE ME

[4] IMPROVED NUMERICAL DISSIPATION FOR TIME INTEGRATION ALGORITHMS IN STRUCTURAL DYNAMICS [J]. EARTHQUAKE ENGINEERING & STRUCTURAL DYNAMICS, 1977, 5 (03) : 283 - 292

[5] A RECURRENCE MATRIX SOLUTION FOR THE DYNAMIC RESPONSE OF ELASTIC AIRCRAFT [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (09): : 540 - &

[6] KATONA MG, 1985, JAN P INT C NUM METH, V1, P213

[7] Lambert J.D., 1973, COMPUTATIONAL METHOD

[8] Newmark N. M., 1959, P AM SOC CIVIL ENG, V8, P67

[9] OSBORNE MR, 1966, BIT, V6, P51

[10] THOMAS R, 1971, 37 U MANCH NUM AN RE

[1] A ONE-STEP METHOD FOR DIRECT INTEGRATION OF STRUCTURAL DYNAMIC EQUATIONS [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1980, 15 (05) : 685 - 699

[2] Dahlquist GG, 1963, BIT, V3, P27, DOI [10.1007/BF01963532, DOI 10.1007/BF01963532]

[3] Henrici P, 1962, DISCRETE VARIABLE ME

[4] IMPROVED NUMERICAL DISSIPATION FOR TIME INTEGRATION ALGORITHMS IN STRUCTURAL DYNAMICS [J]. EARTHQUAKE ENGINEERING & STRUCTURAL DYNAMICS, 1977, 5 (03) : 283 - 292

[5] A RECURRENCE MATRIX SOLUTION FOR THE DYNAMIC RESPONSE OF ELASTIC AIRCRAFT [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (09): : 540 - &

[6] KATONA MG, 1985, JAN P INT C NUM METH, V1, P213

[7] Lambert J.D., 1973, COMPUTATIONAL METHOD

[8] Newmark N. M., 1959, P AM SOC CIVIL ENG, V8, P67

[9] OSBORNE MR, 1966, BIT, V6, P51

[10] THOMAS R, 1971, 37 U MANCH NUM AN RE