Theses and Dissertations
Now showing items 1-4 of 4
Analysis of convertiplane propeller-rotors.
(Cranfield, England: College of Aeronautics, 1962-07-01)
An investigation of pressure fluctuations around a circular cylinder
(College of Aeronautics, 1962-06-01)
An iterative method for finding the transient response of an automatically controlled missile having non-linear stiffness.
(Cranfield, England: College of Aeronautics, 1960-06-01)
An equation of missile motion in the pitching plane was found, assuming a non-linearity in aerodynamic stiffness in the form of a cubic term. An iterative method for approximating the angle-ofattack response to a step ...