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Results: 1-7 |
Results: 7
METHODOLOGY FOR IMPLEMENTING FRACTURE-MECHANICS IN GLOBAL STRUCTURAL DESIGN OF AIRCRAFT
Authors: NEES CD CANFIELD RA
Citation: Cd. Nees et Ra. Canfield, METHODOLOGY FOR IMPLEMENTING FRACTURE-MECHANICS IN GLOBAL STRUCTURAL DESIGN OF AIRCRAFT, Journal of aircraft, 35(1), 1998, pp. 131-138
DISCRETE-TIME, MIXED-NORM CONTROL SYNTHESIS APPLIED TO AIRCRAFT TERRAIN FOLLOWING
Authors: JACQUES DR RIDGELY DB CANFIELD RA
Citation: Dr. Jacques et al., DISCRETE-TIME, MIXED-NORM CONTROL SYNTHESIS APPLIED TO AIRCRAFT TERRAIN FOLLOWING, Journal of guidance, control, and dynamics, 19(5), 1996, pp. 1088-1094
A MATLAB TOOLBOX FOR FIXED-ORDER, MIXED-NORM CONTROL SYNTHESIS
Authors: JACQUES DR CANFIELD RA RIDGELY B SPILLMAN MS
Citation: Dr. Jacques et al., A MATLAB TOOLBOX FOR FIXED-ORDER, MIXED-NORM CONTROL SYNTHESIS, Control systems magazine, 16(5), 1996, pp. 36-44
MULTIVARIATE HERMITE APPROXIMATION FOR DESIGN OPTIMIZATION
Authors: WANG LP GRANDHI RV CANFIELD RA
Citation: Lp. Wang et al., MULTIVARIATE HERMITE APPROXIMATION FOR DESIGN OPTIMIZATION, International journal for numerical methods in engineering, 39(5), 1996, pp. 787-803
FINITE-ELEMENT MODEL TUNING USING AUTOMATED STRUCTURAL OPTIMIZATION SYSTEM SOFTWARE
Authors: COBB RG CANFIELD RA LIEBST BS
Citation: Rg. Cobb et al., FINITE-ELEMENT MODEL TUNING USING AUTOMATED STRUCTURAL OPTIMIZATION SYSTEM SOFTWARE, AIAA journal, 34(2), 1996, pp. 392-399
INTEGRATED STRUCTURAL DESIGN AND VIBRATION SUPPRESSION USING INDEPENDENT MODAL SPACE CONTROL
Authors: CANFIELD RA MEIROVITCH L
Citation: Ra. Canfield et L. Meirovitch, INTEGRATED STRUCTURAL DESIGN AND VIBRATION SUPPRESSION USING INDEPENDENT MODAL SPACE CONTROL, AIAA journal, 32(10), 1994, pp. 2053-2060
DESIGN OF FRAMES AGAINST BUCKLING USING A RAYLEIGH QUOTIENT APPROXIMATION
Authors: CANFIELD RA
Citation: Ra. Canfield, DESIGN OF FRAMES AGAINST BUCKLING USING A RAYLEIGH QUOTIENT APPROXIMATION, AIAA journal, 31(6), 1993, pp. 1143-1149
Risultati: 1-7 |