Theses and Dissertations
A method to calculate the parameters of wings of arbitrary planform
An interactive computer aid for the design and analysis of linear, single input
An investigation into the soot production processes in a gas turbine engine.
Development of graphical Pole-zero, Root-Locus, Bode, Nyquist, and Nichols responses using the OPTSYSX Program.
An analysis of three approaches to the helicopter preliminary design problem.
Design of apparatus for the determination of aerodynamic drag coefficients of automobiles.
Computer program to simulate the lateral-directional response of a high performance aircraft digital electronic flight control system.
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Advisor
Author
Branch Of Service
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Lieutenant, United States Navy (7)
Date Issued
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1984 (7)
Degree
Department
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Aeronautical Engineering (7)