Theses most similar to Experimental investigation of the transient response in pitch of a helicopter (Mallen, Joseph; 1949) read it
Prediction of the aero-elastic force in a labyrinth type seal and its impact on turbomachinery stability
Gans, Bruce E (1983)
- Advisor: Stephen H. Crandall
- Department of Mechanical Engineering
Analysis and error model for a two-degrees-of-freedom elastically supported tuned gyro.
Graham, David Bruce (1972)
- Advisor: Wrigley, Walter
- Department of Aeronautics and Astronautics
- Advisor: Norman D. Ham
- Department of Aeronautics and Astronautics
A coning motion apparatus for hydrodynamic model testing in a non-planar cross-flow
Johnson, David Craig (1989)
- Advisor: Justin E. Kerwin
- Department of Mechanical Engineering; Department of Ocean Engineering
- Advisor: Otto C. Koppen
- Aeronautical Engineering Department
- Advisor: E. E. Larrabee
- Aeronautical Engineering Department
A feasibility study of helicopter vibration reduction by self-optimizing higher harmonic blade pitch control.
Shaw, John, Jr (1967)
- Advisor: Rene H. Miller
- Department of Aeronautics and Astronautics
The effect of biplane combination on airfoil characterisitcs
McDonnell, James S; Zakhartchenko, Constantine L (1926)
- Advisor: Edward P. Warner
- Aeronautical Engineering Department
Response characteristics of the valve controlled hydraulic servo
Lipschutz, Lewis D. (Lewis Drucker) (1943)
- Advisor: Christian E. Grosser
- Department of Mechanical Engineering
Dynamical stability of aeroplanes (with three plates)
Chow, Hou Kun; Clark, Virginius Evans, 1866-; Douglas, Donald W. 1892-1981; Huff, T. H; Hunsaker, Jerome C. (Jerome Clarke), 1886-1984 (1916)
- Advisors: C.H. Peabody; Smithsonian Institution. Hodgkins Fund
- Aeronautical Engineering Department