Computational Study of Aerofoil's Self-Noise When Subject to Leading Edge Jet Blowing Flow Control
DESIGN OF AN EFFICIENT CLIMBING FLIGHT TRAJECTORY FOR A FLAPPING-WING MICRO AIR VEHICLE
OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING
COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM
AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES
NEW ROLL-SPIRAL COUPLING MODE CRITERION FOR HIGH-SPEED VEHICLES
AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
DEVELOPMENT OF A HUMAN PILOTED AIR COMBAT ENGAGEMENT DATABASE
NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING
NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS
Structural damage identification using multi-objective optimization based inverse analysis
LOST CIRCULATION PREDICTION IN SOUTH CHINA SEA USING MACHINE LEARNING AND BIG DATA TECHNOLOGY
KEY TECHNOLOGY AND INDUSTRIAL APPLICATION OF HPHT DRILLING AND COMPLETION IN SOUTH CHINA SEA
WING TWIST OPTIMISATION USING AERODYNAMIC SOLVERS OF DIFFERENT FIDELITY
SINGLE-AISLE AIRLINER DISRUPTION WITH A SINGLE-DECK BLENDED-WING-BODY
STUDY ON THE AERODYNAMIC CHARACTERISTICS OF HIGH-ALTITUDE PROPELLERS WITH PROPLETS
ICAS2016_0190: FORMAL VERIFICATION OF AUTOPILOTS IN UMANNED AIRCRAFT SYSTEMS
TRAJECTORY DESIGN FOR THE PHOBOS AND DEIMOS & MARS ENVIRONMENT SPACECRAFT
Linear Control of Highly Flexible Aircraft Based on Loop Separation (AIAA 2016-3398)
Performance Analysis of a Pure Electric Light Off-Road Vehicle Based on the Cruise
Research of AI Planning for Space Flight Control Based on PDDL
Compressive Sensing for DS TT&C Signals Based on Basic Dictionary Building
Characterizing Wheel Flat Impact Noise with an Efficient Time Domain Model
Solutions for Extracting Air and Smoke in Underground Subway Station
The Co-simulation of Airborne Stable Platform Based on Adams/Simulink
Flight Dynamic Characteristic Analysis of a Generic Airbreathing Hypersonic Vehicle