The Employment of Artificial Intelligence for Analyzing Air Accidents
ICAS-92-3.9.2 The Employment of Artificial Intelligence for Analyzing Air Accidents
High-photosensitivity a-SiGe: H films prepared by RF glow discharge plasma CVD method
Multiple Degree of Freedom Global Analysis of Transient Ship Rolling Motion
Two-Head Detonation Structure in Cornstarch-Oxygen Mixtures
H~ Control Problem for a Plant Possessing Zeros at Infinity
A System to Prevent Liquid Cargo Tanker Pollution and Spill
8 x 8, 0.88-m wavelength of LED matrix module [2321-40]
Compression of the signals of large dynamic range for underwater object laser detection [2321-67]
Numerical and experimental studies of jet flow exhausting from rocket
A novel optical fibre sensor for turbidity measurement
Effect of Miller Cycle on Gas Engine for Generation (9630723)
Diagnosis of the Working Unevenness of Each Cylinder by the Transient Crankshaft Speed
Diagnosis of the working unevenness of each cylinder by the transient crankshaft speed
Investigation of quantum well lasers which have superlattice buffer layer [2886-562]
Block diagonal form and block diagonal controller of nonlinear systems
Effect of EGR on The Late Intake-Valve Closing Miller Cycle for Natural Gas Engines
Improvement of BMEP for Natural Gas Fueled Spark Ignition Engines by Using Miller Cycle and EGR
Replication Control for Fault-Tolerance in Distributed Real-Time Database Systems
The Disposal to Face-based Representation of Design/Manufacturing Feature Integration
Computerized Tomography for Reconstruction of the Parameters of Arcjet Plume
Simulation of Vehicular Emission Features in Terms of Engine Emission Performance
Gasoline Engine Idle Speed Control System Development Based on PID Algorithm
A Micro-processor Based Adaptive Ignition Control System
Improvement of engine vibration isolation characteristics by using semi-active hydraulic mount
Gas pendulum accelerometer and tilt sensor [4414-51]
Euler and Navier Stokes Optimizations of Airfoils Using Genetic Algorithms
Structural principle and property of piezoelectric quartz tilt meter [4414-74]
Numerical Investigation of the Aerodynamic Performance of the Aurora CP-140 Aircraft
Use of Navier-Stokes Methods for Analysis of High-Lift Systems
Ozone sensor with hsgfet and its characteristic [4414-47]
An Micro-Bandpasss (6.37.6mm) Filter for the Multichannel Scanning Radiometer
A Study on Nonlinear Stiffness Characteristic of Air Spring for a Bus
AIAA-2002-5405 Integrated Wing Design with Three Disciplines