MOMENTUM TRANSFER IN MILLISECOND PERIODIC-PULSED DIELECTRIC-BARRIER-DISCHARGE PLASMA ACTUATOR
Boundary-Layer Transition Effects on Aerodynamic Characteristics of AGARD-B Mode
Numerical Computation of Pressure Distributions over Conical Forebody at High Angles of Attack
Visualization of Vortex Flow over Delta Wing with Dorsal Fin
Computational Analysis of Conical Forebody at High Angles of Attack with Transitional Model
Multiple Solutions and Buffet of Transonic Flow over the NACA0012 Airfoil
Flow Control Over a Conical Forebody Using Duty-Cycled Plasma Actuators
All-Fiber Dissipative Solitons Evolution in a Compact Passively Yb-Doped Mode-Locked Fiber Laser
Reply to Comment - "Generalized Technique for Inverse Simulation Applied to Aircraft Maneuvers"
Pressure around a 20-degree Circular Cone at 35-degree Angle of Attack and Low Speed
Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin AIAA Paper
Optical image processing technology in recognizing specific trace [5058-73]
Research on application of special filter in projecting grating profilometry [5058-69]
Calibration algorithm of unequal step phase shifting based on checking [5058-68]