Inductive-Based Machine Learning and the Application in Assessment of Ship Handling
17.8 Intelligent evaluation system of ship management
Designing High Dynamic Range Microwave Photonic Links for Radio Applications
An Active Queue Management (AQM) Scheme Based on Modified Smith Predictor
Efficient broadband simulations for thin optical structures
Vortex Flow Control over a Delta Wing Using Leading-edge Rudder (AIAA 2014-0956)
Flow Control over a Conical Forebody Using Pulsed Nanosecond Discharge Actuators (AIAA 2014-0933)
ENSEMBLE AND PHASE-LOCKED AVERAGED LOADS CONTROLLED BY PLASMA DUTY CYCLES
PIV Study of Conical Forebody Flow Control Using Plasma Actuators
Optimal DBD Duty-Cycle for Conical Forebody Side-Force Proportional Control
Flow Control over Conical Forebody with Port Pulsed Plasma Actuator
Effect of Plasma Actuation on Asymmetric Vortex Flow Over a Slender Conical Forebody
Diode-pumped cw and Q-switched NdGdVO4 laser operating at 1.34 mm
EXPERIMENTAL INVESTIGATIONS ON STABILITY OF VORTEX FLOW OVER SLENDER DELTA WING WITH DORSAL FIN
Study on Properties of the Urea and L-alpha-Alanine Didoped Triglycine Sulfate(UrLATGS) Crystals
Comparison of Pressures Driven by Repetitive Nanosecond Pulses to AC Result (AIAA 2014-0094)
Comparison of Velocities Driven by Repetitive Nanosecond Pulses to AC Result (AIAA 2014-0327)
Asymmetry Features Independent of Roll Angle for Slender Circular Cone
Research and Application of Weighted Apriori Algorithm in Rail Freight Volume Forecasting
Body Force Produced by Plasma Actuator Using PIV and Pressure Measurements
Software control architecture for autonomous vehicles [3693-36]
Construction of Operational Model on Reverse Logistics of Hazardous Waste
Phase transition in ferroelectric hemicyanine Langmuir-Blodgett multilayers [5564-17]
Visualization of Vortex Flow over Delta Wing with Dorsal Fin
Flow Control Over a Conical Forebody Using Duty-Cycled Plasma Actuators
Space Science Mission Operation System Joint Test Method Research
Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin AIAA Paper
Pressure around a 20-degree Circular Cone at 35-degree Angle of Attack and Low Speed