目录
- Theoretical modeling of vectoring dual synthetic jet based on regression analysis
- Flow field generated by a dielectric barrier discharge plasma actuator in quiescent air at initiation stage
- Feedback control of boundary layer Tollmien-Schlichting waves using a simple model-based controller
- Evolution of convex structure during counter-rotating electrochemical machining based on kinematic modeling
- Mathematical modeling of an armature assembly in pilot stage of a hydraulic servo valve based on distributed parameters
- Optimization and verification of wind tunnel free-flight similarity law for separation of cluster munition
- Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number
- Effect of fuel type on the performance of an aircraft fuel tank oxygen-consuming inerting system
- Criteria for hypersonic airbreathing propulsion and its experimental verification
- Effect of scavenge port angles on flow distribution and performance of swirl-loop scavenging in 2-stroke aircraft diesel engine
- Comprehensive optimization design of aerodynamic and electromagnetic scattering characteristics of serpentine nozzle
- Proactive optimization of transmission power and 3D trajectory in UAV-assisted relay systems with mobile ground users
- Ship detection and classification from optical remote sensing images: A survey
- Variational method based robust adaptive control for a guided spinning rocket
- Coordinated attitude control for flexible spacecraft formation with actuator configuration misalignment
- Libration and end body swing stabilization of a parallel partial space elevator system
- Civil unmanned aircraft system operation in national airspace: A survey from Air Navigation Service Provider perspective
- Inertial parameter estimation and control of non-cooperative target with unilateral contact constraint