Add to ORKGThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.Includes bibliographical references (leaves 145-152).by Andrew Man-Chung Wo.Ph.D
Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
In this thesis we describe the development of Reynolds- averaged Navier Stokes code for the flow pas...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
Force and particle image velocimetry measurements were conducted on a NACA 0012 airfoil undergoing s...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
Laser Doppler Velocimeter data, static pressure data, and smoke flow visualization data was obtained...
The differences in flow behavior two dimensional airfoils in the critical chordlength Reynolds numbe...
The results of the research conducted under this grant are presented in detail in three Master these...
This thesis combines experimental and computational methods to investigate the low Reynolds number f...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of General Science, 1928.Includes biblio...
Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...
Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
In this thesis we describe the development of Reynolds- averaged Navier Stokes code for the flow pas...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
Airfoil geometries were developed for low speed high lift applications, such as general aviation air...
Force and particle image velocimetry measurements were conducted on a NACA 0012 airfoil undergoing s...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
Laser Doppler Velocimeter data, static pressure data, and smoke flow visualization data was obtained...
The differences in flow behavior two dimensional airfoils in the critical chordlength Reynolds numbe...
The results of the research conducted under this grant are presented in detail in three Master these...
This thesis combines experimental and computational methods to investigate the low Reynolds number f...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of General Science, 1928.Includes biblio...
Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...
Summary: The collected data for a series of oscillatory pitch tests on a NACA 23012 aerofoil at lo...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...