Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.Title as it appears in the M.I.T. Graduate List, Feb. 1991: Computational investigation of Campbell diffuser concept.Includes bibliographical references (leaves 110-113).by Wai Chung Au.M.S
Theoretical Mach number distributions and boundary-layer parameters are presented for subsonic nacel...
Air entering the engine of a supersonic aircraft must be slowed to subsonic speeds for the engine to...
Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949.Bibliog...
Campbell diffusers have a unique feature in that they lack axial symmetry in the end walls. It has b...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
A finite difference computer program for turbulent compressible flow was used to establish the perfo...
September 1997Includes bibliographical references (pages 81-84)A computational investigation of the ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
A computer design program was developed to incorporate the suction slots in solving the potential fl...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
A survey of external-compression inlets was completed to characterize their basic features including...
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, 1993.In...
This study is aimed at the development of a computational technique for the prediction of the flow f...
Theoretical Mach number distributions and boundary-layer parameters are presented for subsonic nacel...
Air entering the engine of a supersonic aircraft must be slowed to subsonic speeds for the engine to...
Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949.Bibliog...
Campbell diffusers have a unique feature in that they lack axial symmetry in the end walls. It has b...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
A finite difference computer program for turbulent compressible flow was used to establish the perfo...
September 1997Includes bibliographical references (pages 81-84)A computational investigation of the ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
A computer design program was developed to incorporate the suction slots in solving the potential fl...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
A survey of external-compression inlets was completed to characterize their basic features including...
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, 1993.In...
This study is aimed at the development of a computational technique for the prediction of the flow f...
Theoretical Mach number distributions and boundary-layer parameters are presented for subsonic nacel...
Air entering the engine of a supersonic aircraft must be slowed to subsonic speeds for the engine to...
Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949.Bibliog...