°Ekonomičeskie Problemy povyšenija °effektivnosti transportnogo stroitelʹstva
A Computer-Aided Optimization Approach for the Design of Injection Mold Cooling Systems
Adaptarea motorului cu ardere interna la conditile autopropulsarii prin echiparea cu CVT
A Derivation of the Pole Curve Equations in the Projective Plane
Advances in brake system engineering and components : Auto Tech '89 Seminar Papers (C 399-34)
A Feasibility Robust Optimization Method Using Sensitivity Region Concept
A Fuzzy Dynamic Programming Approach for the Mixed-Discrete Optimization of Mechanical Systems
A Generalized Stiffness Matrix Method for Force Distribution of Robotic Systems with Indeterminacy
A Genetic Algorithm for Scheduling and Decomposition of Multidisciplinary Design Problems
A Kriging Metamodel Assisted Multi-Objective Genetic Algorithm for Design Optimization
A Linear Beam Finite Element Based on the Absolute Nodal Coordinate Formulation
American Carrier Air Power at the Dawn of a New Century
American Carrier Air Power at the Dawn of a New Century
A Method to Improve Platform Leveraging in a Market Segmentation Grid for an Existing Product Line
Analysis and Design of Protein Based Nanodevices: Challenges and Opportunities in Mechanical Design
An analysis on Aerodynamics Performance Simulation of NACA 23018 Airfoil Wings on Cant Angles
An Automated Design Search for Single and Double-Planet Planetary Gear Sets
An Energy-Based General Method for the Optimum Synthesis of Mechanisms
A New Class of Six-Bar Mechanisms With Symmetrical Coupler Curves
An Optimization-Based Framework for Simultaneous Plant-Controller Redesign
Application of the Euler method EUFLEX to a fighter-type airplane configuration at transonic speed
Applied Tests of Design Skills-Part 1: Divergent Thinking
A Shape Optimization Method Based on Implicit Differentiation and Node Removal Techniques
A Simulated Annealing-Based Approach to Three-Dimensional Component Packing
Assessing the boundaries of the airport services market: Grounds for tariff deregulation
ASSESSMENT OF RELIABILITY OF THE ONBOARD EQUIPMENT OF SMALL SPACECRAFTS DURING THEIR FLIGHT