Research on the structural performance of large rocket booster subjected to longitudinal excitations
Dynamic structural behavior of large booster rocket subjected to longitudinal excitations - analysis of theoretical model
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Dynamic structural behavior of large booster rocket subjected to longitudinal excitations - analysis of theoretical model
Theoretical models for lunar brightness at small phase angles and polarization of moonlight
Unified theoretical model of hypersonic viscous shock layer for wide range of Reynolds numbers, including mass transfer effects
Choked flow analogy for very low quality two-phase flows - homogeneous flow and hydraulic jump theoretical models for predicting axial pressure distribution
Theoretical model and application of error rate reduction of parity checked telemetry data by likelihood deletion strategy
This is the sixth yearly report on the research at Princeton University on the problem of combustion instability in liquid-propellant rocket motors. These investigations have been sponsored by the National Aeronautics and Space Administration under NASA Contract NASr-217 and, in the past, under NASA Grant NsG-99-60. The nonlinear aspects of the problem have been emphasized in both the theoretical and experimental portions of the program. Presently, the theoretical research primarily involves studies of possible mechanisms or forcing functions of the instabilities, the nonlinear gasdynamic oscillations associated with instability in rocket motors, the effect of the exhaust nozzle on the stability, and the effect of damping devices on the stability. In conjunction with the theoretical program, an experimental program of an equally broad range is being conducted. This program includes basic experiments both with rocket motors and "cold" chambers which have been designed to study various combustion processes in order to provide understanding which would be useful in the construction of a theoretical model. It also includes studies of the effects of exhaust nozzles and damping devices upon the instability as well as controlled testing of liquid rocket motors with parametric variations intended to determine the factors which strongly influence the incidence of nonlinear combustion instability.
Theoretical modeling study of gamma ray scattering technique for measuring atmospheric density
Theoretical models of infrared radiative properties of missile exhaust plumes for long range detection
Ionospheric research from space vehicles, comparing experimental data with theoretical models of D, E and F regions
Theoretical model for effect of mechanical stress on generation-recombination currents in p-n junctions
Measured time-dependent electron velocity in weakly ionized plasma compared with theoretical model using Boltzmann equation
Theoretical model for predicting performance of thin base solid state diode in low current range
Mechanical properties of stryene-butadiene rubber glass bead composites, and theoretical model on isothermal volume dilatation and stress-strain relationship in filler concentration
Astrophysical evidence for direct electron- neutrino weak interaction - theoretical models of superluminous white dwarfs with and without neutrino emission process
Theoretical modeling of fog modification by seeding with hygroscopic nuclei, climatic survey of fog frequency in Buffalo, New York, large scale laboratory experiments, and field tests
Theoretical model for storage and retrieval in long-term memory
Solid state imaging system with silicon phototransistor mosaic achieving 100 line resolution, discussing theoretical model and system imaging performance
Rocket combustion instability studied experimentally using theoretical model characterizing combustion by time lag and interaction index