An unsteady wind tunnel was designed and built for the study of unsteady aerodynamics. The wind tunnel was designed as an open-loop configuration, and an active flow control system was designed as a series of horizontally aligned shutters placed in front of the test section which can block oncoming airflow to create time-varying shear flows in the test section. The wind tunnel was constructed using primarily acrylic and plywood and was run by an axial fan. The active flow control system was composed of four shutters that were held in position and rotated using steel rods and actuators located just outside the shutter frame. Computational Fluid Dynamics (CFD) was used throughout the design processes, ensuring the generation of unsteady flows...
This study is motived by the dynamic stall of rotorcraft blades. Dynamic stall is an attribute of ai...
abstract: This study uses Computational Fluid Dynamics (CFD) modeling to analyze the dependence of ...
Dynamic stall occurs in applications where airfoils are rapidly changing angle of attack, like rotor...
This study investigates potential cost of energy reductions that might be achieved by designing acti...
This study investigated the impact of vane design for a retractable vane Savonius style Vertical Axi...
UnderGraduate Research GrantCounter Rotating Open Rotor (CROR) systems promise a light weight, fuel ...
The power generation by a Horizontal Axis Wind Turbine (HAWT) is considered to be at the forefront o...
Aerodynamic drag accounts for a sizable portion of transportation energy consumption. Transportatio...
This project involved the analysis, design, and fabrication of an aircraft meeting the requirements ...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
Separation of flow from the surface of an airfoil is a great limiting factor in the development of a...
This project furthers the design and testing of the WPI kite-powered water-pump system. The purpose ...
The objective of this thesis was to develop an experimental method to research circulation control w...
Increased interest in launching nanosatellites drives the development of alternative, more efficient...
A new 3"x3" supersonic wind tunnel was built to facilitate the continued development of localized ar...
This study is motived by the dynamic stall of rotorcraft blades. Dynamic stall is an attribute of ai...
abstract: This study uses Computational Fluid Dynamics (CFD) modeling to analyze the dependence of ...
Dynamic stall occurs in applications where airfoils are rapidly changing angle of attack, like rotor...
This study investigates potential cost of energy reductions that might be achieved by designing acti...
This study investigated the impact of vane design for a retractable vane Savonius style Vertical Axi...
UnderGraduate Research GrantCounter Rotating Open Rotor (CROR) systems promise a light weight, fuel ...
The power generation by a Horizontal Axis Wind Turbine (HAWT) is considered to be at the forefront o...
Aerodynamic drag accounts for a sizable portion of transportation energy consumption. Transportatio...
This project involved the analysis, design, and fabrication of an aircraft meeting the requirements ...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
Separation of flow from the surface of an airfoil is a great limiting factor in the development of a...
This project furthers the design and testing of the WPI kite-powered water-pump system. The purpose ...
The objective of this thesis was to develop an experimental method to research circulation control w...
Increased interest in launching nanosatellites drives the development of alternative, more efficient...
A new 3"x3" supersonic wind tunnel was built to facilitate the continued development of localized ar...
This study is motived by the dynamic stall of rotorcraft blades. Dynamic stall is an attribute of ai...
abstract: This study uses Computational Fluid Dynamics (CFD) modeling to analyze the dependence of ...
Dynamic stall occurs in applications where airfoils are rapidly changing angle of attack, like rotor...