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The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System
Robust Adaptive Fault-Tolerant Control for Hypersonic Flight Vehicles with Multiple Faults
Fault Early Recognition and Health Monitoring on Aeroengine Rotor System
System Design and Analysis Methods
Dynamics of Spring-Deployed Solar Panels for Agile Nanospacecraft
Heat Treatment Martensitic Corrosion-Resistant Steel Parts
Steel, Corrosion and Heat-Resistant, Welding Wire 16.5Cr - 4.5Ni - 2.9Mo - 0.10N
Vibration Transfer Path Analysis of Aeroengines Using Bond Graph Theory
Crashworthiness Performance Simulation and Analysis of Combined-Type Landing Gear Buffer
Sliding Mode Reconfigurable Fault Tolerant Control for Nonlinear Aircraft Systems
The Verification of the Technical Conditions of a Combat-Trainer Jet’s Airframe
Quasi-One-Dimensional Numerical Method for Solid Fuel Scramjet Combustor Analysis and Design
Improved Thermal and Vertical Trajectory Model for Performance Prediction of Stratospheric Balloons
Investigation of Panel Flutter under the Effect of Liquid Sloshing
Aircraft Propulsion Health Management
IFF Optimal Control for Missile Formation Reconfiguration in Cooperative Engagement
Modeling and Contribution Analysis of Vibration Transfer Paths for a Dual-Rotor Aeroengine
Steel, Corrosion and Heat-Resistant, Welding Wire 19Cr - 12.5Ni - 2.5Mo
Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and Higher
Design of a Lunar Surface Structure. II: Seismic Structural Analysis
Evaluation of Impact Damage in Composite Structures Using Ultrasonic Testing
Sun-Seeking Eternal Flight Solar-Powered Airplane for Venus Exploration
Design of a Lunar Surface Structure. I: Design Configuration and Thermal Analysis
Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and Higher
Design and Characterization of a Space-Based Imaging Experiment Computer Unit
Adaptive Tuning of the Unscented Kalman Filter for Satellite Attitude Estimation
Aerodynamic Interference Issues in Aircraft Directional Control
Evaluation of the Modified Picard-Chebyshev Method for High-Precision Orbit Propagation
Adaptive Control of Shock Waves with a Passively Morphing Layer for Rotating Blades
Influence of Strake Wing on Unsteady Characteristics of an Aircraft Undergoing Lateral Motions
Heat Treatment of Low-Alloy Steel Parts Minimum Tensile Strength 220 ksi (1517 MPa) and Higher
Model predictive control for space teleoperation systems based on a mixed- approach
Aluminum Alloy, Castings 5.0Si - 1.2Cu - 0.50Mg (355.0-T51) Precipitation Heat Treated
Attitude and Momentum Management of Inertial Oriented Spacecraft