Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.Title as it appears in the M.I.T. Graduate List, Sept. 1989: Blade row interaction effect on compressor measurement.Includes bibliographical references (leaves 34-36).by Tonghuo Shang.M.S
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, Febru...
This paper details an experimental investigation, using a linear cascade, into the effects of real g...
The effects of blade row interactions on stator-mounted instrumentation in axial compressors are inv...
Although it is known that the flow field in a turbomachine is unsteady, current design tools do not ...
The performance of compressors and the sophistication of analysis tools have reached a level such th...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.Includes...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Steady state, inter row measurements in multistage axial compressors are relevant to the current de...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
Presented at the International Gas Turbine and Aeroengine Congress and Exposition Orlando, FL June ...
While the gas turbine engine has existed for nearly 80 years, much of the complex aerodynamics which...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001....
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, Febru...
This paper details an experimental investigation, using a linear cascade, into the effects of real g...
The effects of blade row interactions on stator-mounted instrumentation in axial compressors are inv...
Although it is known that the flow field in a turbomachine is unsteady, current design tools do not ...
The performance of compressors and the sophistication of analysis tools have reached a level such th...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.Includes...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
Steady state, inter row measurements in multistage axial compressors are relevant to the current de...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.In...
Presented at the International Gas Turbine and Aeroengine Congress and Exposition Orlando, FL June ...
While the gas turbine engine has existed for nearly 80 years, much of the complex aerodynamics which...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001....
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, Febru...
This paper details an experimental investigation, using a linear cascade, into the effects of real g...
The effects of blade row interactions on stator-mounted instrumentation in axial compressors are inv...