Add to ORKGThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.Includes bibliographical references (leaves 225-233).by Norman Kai Wing Lee.Ph.D
A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender ...
The vortex dynamics of leading-edge vortices on plunging high-Aspect-ratio (ARÂ =Â 10) wings and air...
A review of leading edge vortex studies conducted at the University of Notre Dame is presented. The ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990....
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994....
Prepared by Cornell Aeronautical Laboratory, Inc., for Langley Research Center.N 71-34004.Includes b...
Micro air vehicles are used in a myriad of applications, such as transportation and surveying. Their...
The dye injection and hydrogen bubble visualization techniques are used to investigate the dual-vort...
<p>Vortex structures are identified by plotting an isosurface of the imaginary part of the complex e...
Prepared at the Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, for Ames Re...
By varying leading edge geometry to wing profiles during flapping flight, Ozen and Rockwell observed...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Earth, Atmosphere and Planetary Sci...
In the more than three decades of research on the lee surface flow of delta wings, starting from the...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Ocean Engineering, 1991.Includes bibl...
A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender ...
The vortex dynamics of leading-edge vortices on plunging high-Aspect-ratio (ARÂ =Â 10) wings and air...
A review of leading edge vortex studies conducted at the University of Notre Dame is presented. The ...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990....
The structure of the leading-edge vortex from a delta wing at high angle of attack is addressed usin...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994....
Prepared by Cornell Aeronautical Laboratory, Inc., for Langley Research Center.N 71-34004.Includes b...
Micro air vehicles are used in a myriad of applications, such as transportation and surveying. Their...
The dye injection and hydrogen bubble visualization techniques are used to investigate the dual-vort...
<p>Vortex structures are identified by plotting an isosurface of the imaginary part of the complex e...
Prepared at the Dept. of Aerospace and Mechanical Engineering, University of Notre Dame, for Ames Re...
By varying leading edge geometry to wing profiles during flapping flight, Ozen and Rockwell observed...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Earth, Atmosphere and Planetary Sci...
In the more than three decades of research on the lee surface flow of delta wings, starting from the...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Ocean Engineering, 1991.Includes bibl...
A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender ...
The vortex dynamics of leading-edge vortices on plunging high-Aspect-ratio (ARÂ =Â 10) wings and air...
A review of leading edge vortex studies conducted at the University of Notre Dame is presented. The ...