Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.Includes bibliographical references (leaves 86-88).by Michael R. D'Angelo.M.S
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Turbulent trailing edge flow over control surfaces continues to be of interest to many designers and...
Summary: This paper presents a method for assessing two-dimensional aerofoil performance charact...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
DNS of the flow fi eld around a NACA 0012 airfoil at Re = 50,000 and angle of attack 5 degrees with ...
Direct numerical simulations of the flow field around a NACA 0012 airfoil at Reynolds number 50 000 ...
Summary: This paper presents a method for assessing two-dimensional aerofoil performance charact...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994....
Summary: Little is known about the detailed flow on the upper surface of aerofoils, prone to trai...
The viscous flow phenomena associated with sharp and blunt trailing edge airfoils were investigated....
A new interacting boundary layer approach for computing the viscous transonic flow over airfoils is ...
A low speed airfoil design and analysis program was developed which contains several unique features...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990....
A study has been made on the influence of the open trailing edge in airfoils used in different devic...
An algorithm for estimating the lift, moment and pressure distribution on arbitary two dimensional ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Turbulent trailing edge flow over control surfaces continues to be of interest to many designers and...
Summary: This paper presents a method for assessing two-dimensional aerofoil performance charact...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
DNS of the flow fi eld around a NACA 0012 airfoil at Re = 50,000 and angle of attack 5 degrees with ...
Direct numerical simulations of the flow field around a NACA 0012 airfoil at Reynolds number 50 000 ...
Summary: This paper presents a method for assessing two-dimensional aerofoil performance charact...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994....
Summary: Little is known about the detailed flow on the upper surface of aerofoils, prone to trai...
The viscous flow phenomena associated with sharp and blunt trailing edge airfoils were investigated....
A new interacting boundary layer approach for computing the viscous transonic flow over airfoils is ...
A low speed airfoil design and analysis program was developed which contains several unique features...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990....
A study has been made on the influence of the open trailing edge in airfoils used in different devic...
An algorithm for estimating the lift, moment and pressure distribution on arbitary two dimensional ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Turbulent trailing edge flow over control surfaces continues to be of interest to many designers and...
Summary: This paper presents a method for assessing two-dimensional aerofoil performance charact...