An Investigation of Hypersonic Flow Separation and Control Characteristics
Fin Buffeting Characteristics of a Generic Single Fin Aircraft
Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6.80
Detached-Eddy Simulations of Full Aircraft Experiencing Massively Separated Flows
Investigation by Particle Image Velocimetry Measurements of Oblique Shock Reflection with Separation
Computation of Shock Cell Structure of Dual-Stream Jets for Noise Prediction
Delayed Detached-Eddy Simulation and Analysis of Supersonic Inlet Buzz
Novel Kevlar-Walled Wind Tunnel for Aeroacoustic Testing of a Landing Gear
Flow Reattachment and Vortex Re-formation on Oscillating Low-Aspect-Ratio Wings
Detached-Eddy Simulation Around a Forebody with Rotary Motion
Alleviation of Pressure Rise from a High-Speed Train Entering a Tunnel
Lift Response of a Stalled Wing to Pulsatile Disturbances
Aerodynamic Stall Suppression on Aerofoil Sections Using Passive Air-Jet Vortex Generators
Two-Dimensional Visualization of Turbulent Wall Shear Stress Using Micropillars
Airfoil Stall Suppression by Use of a Bubble Burst Control Plate
Smoke-Wire Flow Visualization in Separated Flows at Relatively High Velocities
Aero-Micro-Electromechanical System Sensor Arrays for Time Resolved Wall Pressure Measurements
Three-Dimensional Analysis of a Supersonic Combustor Coupled to Innovative Inward-Turning Inlets
Jet Entrainment Theory for Vertical Takeoff and Landing Aircraft Suckdown
Investigation of the Taylor-Culick Flow Through Particle Image Velocimetry and Numerical Simulation
Computation of Wall Pressure Spectra from Steady Flow Data for Noise Prediction
Yaw Angle Effect on Flow Structure over the Nonslender Diamond Wing
Influence of Reynolds Number on Vortex Flow over a Non-slender Delta Wing
Effect of Pitch Rate on Near-Surface Topology on a Delta Wing
Closed-Loop Control of Vortex Formation in Separated Flows with Application to Micro Air Vehicles
Effects of Oxygen Content on Dielectric Behavior Barrier Discharge Plasma Actuator Behavior
Control of Separated Flow over Swept Missile Fin Using Pitching Oscillations
Blowing Effects on the Separated Flow over a Moderately Swept Missile Fin
Near-Wall Formulation of the Partially Averaged Navier Stokes Turbulence Model
Evaluation of a Vortex Generator Model in Adverse Pressure Gradient Boundary Layers
Extension and Exploration of a Hybrid Turbulence Model on Unstructured Grids
Aerodynamic Characteristics at Low Reynolds Number for Wings of Various Planforms
Central Recirculation Zone Visualization in Confined Swirl Combustors for Terrestrial Energy
Control of a Shock/Boundary-Layer Interaction by Using a Pulsed-Plasma Jet Actuator
Minimizing the Loss Produced by a Turbulent Separation Using Vortex Generator Jets
Body Force Model for the Aerodynamics of Inclined Perforated Surfaces
Large-Eddy Simulation of Shock/Boundary-Layer Interaction
Wall Pressure Unsteadiness and Side Loads in Overexpanded Rocket Nozzles
Numerical Investigation to Forcing Frequency and Amplitude of Synthetic Jet Actuators
Improved Stall-Delay Model for Horizontal-Axis Wind Turbines
Active Flow-Separation Control on a High-Lift Wing-Body Configuration
Abort Separation of Launch Escape System Using Aerodynamic Interference