Nucleosynthetic vanadium isotope heterogeneity of the early solar system recorded in chondritic meteorites
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SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Combustion instability in liquid propellant rocket motors causing pressure fluctuations
Spheroidal-type seismogram study of wave generation, propagation, dispersion and attenuation in realistic spherical Earth models, especially Gutenberg-Bullen A-prime model
Impurity effects on nucleation of Se vapor onto Pyrex glass noting degree of critical supersaturation, production of phase with nonequilibrium structure, etc
Bi and Ag nucleation on evaporated substrates studied as function of substrate temperature and impinging flux using electron microscopy
Spontaneous ignition temperature, ignition temperature, and transition temperature for metal-oxidizing gas system models of solid propellant rocket engine combustion processes
Computer program for solutions to equilibrium and nonequilibrium chemical state relations for open and closed thermodynamic systems
Pulsed ruby laser mass spectrometry technique for flash pyrolysis of ammonium perchlorate-catalyst mixtures
Thermal accommodation coefficient and critical supersaturation for nucleation of mercury vapor on pyrex glass
Thermodynamics and kinetics of sublimation, catalytic, and oxidation reactions
Confined turbulent mixing of dissimilar jets in initial region
Dissimilar coaxial axisymmetric jets confined laminar mixing obtained from numerical solution of boundary layer equations, considering binary, isothermal and nonreacting system
Pulsed ruby laser mass spectrometry technique for flash pyrolysis of ammonium perchlorate-catalyst mixtures
Propellant low temperature preignition reactions during simulated engine shutdown conditions, discussing IR spectroscopic observation method
Decane and hexadecane fog detonation propagation in gaseous oxygen
Development of a combustion theory based on the laminarized solutions to the energy and flow conservation equations, which is more realistic in recognizing the nature of the heating-rate problem and in obtaining a practical solution to estimating its magnitude. A new experimental approach is used for studying the combustion behavior of pure monopropellants and composite propellants which uses a laser beam to supply additional heat feedback to a burning surface. New experimental data are presented for the laser-induced combustion rate and ignition delay of pure ammonium perchlorate. The pure monopropellant theory is generalized to include such nonadiabatic effects, and the new experimental data are in good agreement with the nonadiabatic theory.-
Consideration of coupled stress waves generated by an impulsive load applied at one end of a semiinfinite plate. For the field equations governing the one-dimensional coupled waves a hyperbolic system of equations is obtained in which a strong coupling in the second derivatives exists. The method of characteristics described by Chou and Mortimer (1967) is extended to cover the case of strong coupling, and a study is made of the transient stress waves in a semiinfinite plate subjected to an initial step input. Coupled discontinuity fronts are found to propagate at different velocities. The normal plate stress and the bending moment at different time regimes are illustrated by graphs.