目录
- A general method for closed-loop inverse simulation of helicopter maneuver flight
- Numerical simulation of a cabin ventilation subsystem in a space station oriented real-time system
- Parametric analyses on dynamic stall control of rotor airfoil via synthetic jet
- Effect of particle size and oxygen content on ignition and combustion of aluminum particles
- Effects of axial gap and nozzle distribution on aerodynamic forces of a supersonic partial-admission turbine
- Effect of a transverse plasma jet on a shock wave induced by a ramp
- Numerical study of aircraft wake vortex evolution near ground in stable atmospheric boundary layer
- Unsteady supercritical/critical dual flowpath inlet flow and its control methods
- Aeroelastic stability of full-span tiltrotor aircraft model in forward flight
- Control method for multi-input multi-output non-Gaussian random vibration test with cross spectra consideration
- Compressive failure analysis of unidirectional carbon/epoxy composite based on micro-mechanical models
- Nonlinear response analysis and experimental verification for thin-walled plates to thermal-acoustic loads
- A man-made object detection algorithm based on contour complexity evaluation
- Deterministic bound for avionics switched networks according to networking features using network calculus
- Evasion and pursuit guidance law against defended target
- Helicopter blades running elevation measurement using omnidirectional vision
- Three-dimensional adaptive finite-time guidance law for intercepting maneuvering targets
- Effects of pore structure and distribution on strength of porous Cu-Sn-Ti alumina composites
- An optimal method of posture adjustment in aircraft fuselage joining assembly with engineering constraints
- Hybrid task priority-based motion control of a redundant free- floating space robot