目录
- APPLICATION OF HYBRID GENETIC ALGORITHM IN AEROELASTIC MULTIDISCIPLINARY DESIGN OPTIMIZATION OF LARGE AIRCRAFT
- PARAMETRIC MODELING OF COMPONENT LIBRARY FOR LANDING GEAR BASED ON CATIA／CAA
- SMOOTHNESS INDICATOR OF WENO SCHEME FOR RESOLVING SHORT WAVE
- SIMULATION OF BLEED AIR BEHAVIOR DURING AIRCRAFT IN FLIGHT BASED ON FLOWMASTER
- HYBRID AIRFOIL DESIGN FOR FULL-SCALE ICE ACCRETION TEST
- STRAIGHTFORWARD MULTI-SCALE BOUNDARY ELEMENT METHOD FOR GLOBAL／LOCAL MECHANICAL ANALYSIS OF ELASTIC HETEROGENEOUS MATERIAL
- SIMULATION OF TEMPERATURE FIELD IN ULTRA-HIGH FREQUENCY INDUCTION HEATING AND VERIFICATION
- DISCONTINUOUS GALERKIN TIME DOMAIN METHOD FOR SOI THIN-RIDGE WAVEGUIDE PROBLEM
- IMPROVED DOPPLER WARPING METHOD FOR AIRBORNE RADAR WITH NON-SIDELOOKING ARRAY
- MINIMUM ATTRIBUTE CO-REDUCTION ALGORITHM BASED ON MULTILEVEL EVOLUTIONARY TREE WITH SELF-ADAPTIVE SUBPOPULATIONS
- OUTPUT MAXIMIZATION CONTROL FOR VSCF WIND ENERGY CONVERSION SYSTEM USING EXTREMUM CONTROL STRATEGY
- ACTIVE VIBRATION CONTROL OF TWO-BEAM STRUCTURES
- FLEXURAL CAPACITY OF RC BEAM STRENGTHENED WITH PRESTRESSED C／AFRP SHEETS
- MULTI-OBJECTIVE PROGRAMMING FOR AIRPORT GATE REASSIGNMENT
- CALCULATION FOR KERNEL OF INTERVAL GREY NUMBER BASED ON BARYCENTER APPROACH