Add to ORKGThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.Includes bibliographical references (leaves 53-55).by Richard Eugene Kehl.M.S
The objective of the program is to evaluate and develop existing constitutive models for use in fini...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Civil Engineering, 1992.Includes bi...
Current gas turbine engines utilize large single crystal superalloy components in the hot section. S...
Thesis. 1976. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Mi...
Finite element method computer program for solution of stress distribution in plane elastic continu
Unified constitutive material models were developed for structural analyses of aircraft gas turbine ...
An intensive study of the assumed variable distribution necessary for the Assumed Displacement Formu...
When a uniform flow of any nature is interrupted, the readjustment of the flow results in concentrat...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Civil Engineering, 1967.Includes bi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1997.Includes...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
Combined stress theory coupled with laboratory practice has improved student comprehension in both a...
Accomplishments are described for the 2-year program, to develop advanced 3-D inelastic structural s...
The objective of the program is to evaluate and develop existing constitutive models for use in fini...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Civil Engineering, 1992.Includes bi...
Current gas turbine engines utilize large single crystal superalloy components in the hot section. S...
Thesis. 1976. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Mi...
Finite element method computer program for solution of stress distribution in plane elastic continu
Unified constitutive material models were developed for structural analyses of aircraft gas turbine ...
An intensive study of the assumed variable distribution necessary for the Assumed Displacement Formu...
When a uniform flow of any nature is interrupted, the readjustment of the flow results in concentrat...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Civil Engineering, 1967.Includes bi...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1997.Includes...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
Combined stress theory coupled with laboratory practice has improved student comprehension in both a...
Accomplishments are described for the 2-year program, to develop advanced 3-D inelastic structural s...
The objective of the program is to evaluate and develop existing constitutive models for use in fini...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Civil Engineering, 1992.Includes bi...
Current gas turbine engines utilize large single crystal superalloy components in the hot section. S...