Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.Includes bibliographical references (leaves 73-74).by Chiang-Hwa Ren.M.S
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
The configuration and performance of the propulsion system for the hypersonic research vehicle are d...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
A computational parametric investigation was conducted to study the effect of variations to several ...
A computational parametric investigation was conducted to study the effect of variations to several ...
A computational parametric investigation was conducted to study the effect of variations to several ...
Thesis (M.Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997....
A computer program was developed to describe the performance of ramjet and scramjet cycles. The prog...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
The configuration and performance of the propulsion system for the hypersonic research vehicle are d...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
A computational parametric investigation was conducted to study the effect of variations to several ...
A computational parametric investigation was conducted to study the effect of variations to several ...
A computational parametric investigation was conducted to study the effect of variations to several ...
Thesis (M.Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997....
A computer program was developed to describe the performance of ramjet and scramjet cycles. The prog...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The supersonic combustion ramjet or scramjet, is the most suitable engine cycle for sustained hypers...
The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1988.In...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.In...
The configuration and performance of the propulsion system for the hypersonic research vehicle are d...