Topics in aerospace research are presented. They include theoretical and experimental performance of a dual mode ramjet for the Mach 3.5 to 7 domain of flight velocities, time dependent methods for computing wall effects in two-dimensional supercritical flow, analog (rheoelectrical) simulation of the small perturbation equation for transonic flows, determination of the dynamic characteristics of an aircraft structure, and a piston unit for rate modulation of a liquid propellant flow.
Aerospace Research
1974
123 pages
Report
No indication
English
NTIS | 1991
NTIS | 1994
Aerospace materials research project
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