Oscillation periods of neutron stars.
Effect of three-body nuclear potential and two neutron-neutron potentials on radial oscillation periods of neutron stars
OSCILLATION FREQUENCY↗
SEARCH · Engineering Papers
Results for “three body”
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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Recombination and meteor trail decay.
Three-body recombination and meteor trail decay compared with results of afterglow in laboratory plasma
PLASMA DECAY↗
Study compares methods for the numerical solution of ordinary differential equations
Study compares the use of five different methods for the computer solution of the restricted three-body problem. It describes the implementation of each method on a burroughs B-5000 computer and in terms of speed and accuracy.
Source record↗
Virtual mass technique for computing space trajectories Final report
Virtual Mass Technique for computing spacecraft trajectories and Fortran IV computer program for related restricted three-body problem
SPACECRAFT TRAJECTORY↗
Research Achievements Review Series no. 20 - Mathematics and computation research
Computational mathematics, perturbed orbit three-body problem, and periodic trajectories solutions through computer methods
COMPUTER PROGRAMMING↗
New one-step integration methods of high accuracy
New numerical methods for solution of restricted three-body problem periodic trajectories and factors affecting accuracy and computer time through use of new methods
TRAJECTORY ANALYSIS↗
Nonadditivity of intermolecular forces - Effects on the third virial coefficient
Effects of nonadditive three body forces on third virial coefficient
VIRIAL THEOREM↗
Reconsideration of electron attachment rate measurements in the lower ionosphere.
Altitude dependent electron attachment rates and molecular oxygen concentrations indicating three- body attachment process in lower ionosphere
ELECTRON ATTACHMENT↗
Population of atomic levels by dielectronic recombination.
Population of atomic levels by cascade, dielectric and three-body electronic recombination, discussing spontaneous transition, electron impact and RF spectra
EMISSION SPECTRUM↗
Optimized computation with recursive power series integration
Optimized computation with recursive power series integration, applied to three body problem
Estes, R. H.↗
On the application of spinors to the problems of celestial mechanics
Vectorial concept for solving three body problem in celestial mechanics
Stumpff, K.↗
Measurement of ionic recombination rate of nitrogen.
Electron-ion three body recombination rate in nonequilibrium dense nitrogen plasma measured spectroscopically
Park, C.↗
Derivation of a general perturbation solution - Its application to determination of orbit
Analytical solution to three-body problems is applied to the problem of predicting the orbit of a lunar satellite and determining the orbit of a near-earth satellite. Using this solution, the state vector may be generated at any time without intermediate numerical extrapolation.
Born, G. H.↗
Survey of a second class of orbits in the Earth-Moon field - X sub R equals 1.00
Earth-moon field orbit representation by restricted three-body problem and comparison with rotating Kepler orbits
Hoelker, R. F.↗
Variation of parameters and the long-term behavior of planetary orbiters. Part 1 - Theory
Three body problem of planetary orbiters based on central body oblateness, solar effects, and atmospheric drag using equations of motion and transformations
Kaufman, B.↗
Rate constant for deuterium atom recombination calculated by the orbiting resonance theory
Resonance theory for three body recombination kinetics for calculating recombination rate constant of deuterium atom
Bernstein, R. B.↗
Note on a statement in A. Wintner's analytical foundations of celestial mechanics
Disproof of Wintner analytical foundations of celestial mechanics regarding binary collision in three body problem
Sperling, H. J.↗
Mean motions and characteristics exponent at the libration points
Solar system planetary mean motions calculation from characteristic equations roots at equilibrium points of restricted three body problem, using Taylor series solution
Cochran, J. E.↗