Pressure dependence of carbon trioxide formation in the gas-phase reaction of O/D1/ with carbon dioxide
Pressure effects on quantum yields of carbon trioxide formation in gas phase ozone photolysis with carbon dioxide
Dede, C.↗
SEARCH · Engineering Papers
Results for “Pressure effects”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Hypersonic viscous flows
Two dimensional hypersonic viscous flow, analyzing viscosity and bluntness induced pressure effects
Henderson, A., Jr.↗
Thermal conductivity of particulate basalt as a function of density in simulated lunar and Martian environments
Thermal conductivity of particulate basalt as function of density in simulated lunar and Martian environments, noting temperature and pressure effects
Fountain, J. A.↗
The processing of human wastes by wet oxidation for manned spacecraft
Spacecraft wet oxidation for human waste processing, discussing temperature and gas pressure effects, catalyst types, pump requirements, etc
Jaffe, R. J.↗
A kinetic study of the fluorination of silver
Silver fluorination kinetics, taking temperature and pressure effects into account
Odonnell, P. M.↗
Slope discontinuities in pressure vessels
Shell of revolution /pressure vessel/ with meridional slope discontinuity, calculating pressurization effect on stresses by computer program
Skogh, J.↗
Calculated pressure-induced vibrational absorption in H2-H2 collisions in hydrogen gas
Pressure effects on high temperature vibrational absorption coefficients for atomic hydrogen collisions in hydrogen gas
Patch, R. W.↗
Composition gradients in Ni-Fe alloy films produced by vapor deposition from a tungsten boat
Ni-Fe alloy films composition gradients produced by W boats evaporation, noting vapor pressures effect
Carson, K. R.↗
Structural analysis of a solid propellant motor under axisymmetric thermal and pressure loading
Solid propellant engine structural analysis, examining transient thermal loading and internal pressure effects
Chen, J. C.↗
Reactions near the burning surface of double- base propellants
Reaction heat for flameless combustion of double- base propellant using differential scanning calorimetry and thermogravimetric analysis, noting pressure effects
Kirby, C. E.↗
Effect of random fluctuations in pressure gradient on channel flow
Stationary Gaussian Markovian form randomly fluctuating pressure gradient effects on steady incompressible channel flow velocity
Perlmutter, M.↗
Acoustic liner design from a fluid mechanics approach
Acoustic liner design for propellant combustion instability and jet aircraft noise suppression, discussing cross flow and oscillatory pressure effects
Harrje, D. T.↗
Imperfection sensitivity of axially compressed stringer reinforced cylindrical panels under internal pressure
Longitudinal edge stiffness and internal pressure effects on buckling and initial postbuckling behavior of axially compressed stringer reinforced cylindrical panels, discussing imperfection sensitivity
Stephens, W. B.↗
Photographic study of solid propellants burning in an acceleration environment
Photographic study of acceleration and pressure effects on Al agglomerates and combustion processes on solid propellant surface, describing pit growth by combustion model
Baker, K. L.↗
Physical limitations in sensors for a drag-free deep space probe
The inner perturbing forces acting on sensors were analyzed, taking into account the technological limitations imposed on the proof mass position pickup and proof mass acquisition system. The resulting perturbing accelerations are evaluated as a function of the drag-free sensor parameters. Perturbations included gravitational attraction, electrical action, magnetic action, pressure effects, radiation effects, and action of the position pickup. These data can be used to study the laws of guidance, providing an optimization of the space probe as a whole.
Juillerat, R.↗
Infrared laboratory studies of synthetic planetary atmospheres
The initial stages of the research were involved with a test of Burch's law of multiplicative transmittance for mixed absorbing gases when their lines are broadened by H2 and He, which are constituents of the atmospheres of the major planets. The broadening of individual lines in the CO fundamental by various gases was investigated. Line strength and half-width for individual CO lines were studied as a function of temperature. Measurements of total band absorptance as a function of absorber thickness and total effective pressure were made at various temperatures for bands of CO and N2O. Attempts were made to develop a phenomenological theory of line broadening that would account for the phenomena observed for the CO fundamental and those reported for more highly polar gases. Laboratory measurements of nitric acid vapor absorptance were compared with balloon measurements in arriving at an estimate of the quantity of nitric acid vapor present in the earth's atmosphere in the region of the ozone layer.
Williams, D.↗
Short-time oxidation of zirconium.
Study of zirconium oxidation kinetics for maximum exposure times of 3 min and in the temperature range 440 to 850 C. 'Discontinuous' oxidation runs were employed whereby a specimen was inserted into the gas stream for a predetermined time, removed and weighed, and reinserted into the oxidation atmosphere. It is considered that the increase in the observed activation energy for the early stage parabolic oxidation is a manifestation of a change from an n-type oxide to a predominantly p-type oxide, in agreement with the authors' earlier conclusion (1971) based on pressure effects.
Srivastava, L. P.↗
Temperature and pressure dependence of CO2 extinction coefficients.
Results are presented of CO2 extinction coefficient measurements that were performed under conditions of temperature and pressure different from those used by previous investigators. The results show that, whereas pressure effects are generally negligible, temperature dependence is strong enough to invalidate the use of room temperature data for the Mars atmosphere.
Demore, W. B.↗