Optimum design of eccentrically loaded columns.
Eccentrically loaded columns optimum design for minimum volume by interaction method, considering secondary bending and inelastic buckling
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Eccentrically loaded columns optimum design for minimum volume by interaction method, considering secondary bending and inelastic buckling
Stability analysis of highly eccentric satellite orbits about earth in lunar-solar gravitational disturbing field, deriving approximate criteria from planetary perturbation theory
Instability of eccentrically stiffened cylindrical shells under axial compression and lateral pressure
Elastic curve of rotating shaft with vibrations caused by eccentrically located point masses
Misalignment and eccentricity effect on face seal, discussing leakage dependence on phase angle
Exact analytic solution for thermal conductance of two dimensional eccentric constriction in dimensionless numbers
Practical stability of highly eccentric orbits quasi-normal to ecliptic, discussing parameters influence on orbital lifetime with reference to approximate stability criteria
Statistical error analysis of autonomous manned spacecraft navigation in long duration eccentric Mars orbits
Ephemeris of eccentric orbit of Explorer 28
Transient temperature profiles and thermal stress distribution in circular plates and cylinders with eccentric hole determined by conformal mapping
Misalignment and eccentricity effect on face seal, discussing leakage dependence on phase angle
Statistical error analysis of autonomous manned spacecraft navigation in long duration eccentric Mars orbits
Resonant and nonresonant satellite eccentric orbits for determination of high order terms in geopotential
Practical stability of highly eccentric orbits quasi-normal to ecliptic, discussing lunar effects on orbital lifetime
Accelerated longitude drift regimes of eccentric 12 hour orbits due to resonant geopotential
Criticism of Deprit and Rom's (1970) extension of Brouwer's (1959) first-order satellite theory to the third order in J sub 2. It is noted that Deprit and Rom's theory suffers from the drawback that the perturbations of all orders are expressed as infinite power series in the eccentricity e. It is demonstrated that Deprit and Rom's reported failure to extend Brouwer's theory to the second order in a closed form by means of Lie transforms is due to an oversight and is not caused by difficulties inherent in the problem or in the particular perturbation method used.
The accelerated longitude drift regimes of eccentric 12-hr orbits are considered, due to the resonant geopotential. These quasi-stationary orbits are under investigation at NASA for large payload earth surveillance spacecraft in the small applications technology satellite (SATS) program. Inclinations near 'critical' are especially attractive because of their possible long term stability, and these are examined in detail. 'Stable' equator crossing longitudes for these satellites are found as functions of the argument of perigee. As long as the argument of perigee is between plus or minus 100 deg, these stable longitudes lie within a narrow range. Maximum 'east-west' stationkeeping requirements for these satellites at nonequilibrium positions are in the range of 0.3 to 3 m/sec/yr.
The results of some recent work conducted by Anderson (1972) are considered. If Anderson is correct in his conclusion that the bulk composition of the moon resembles that of the Allende inclusions, then the natural place for the formation of the moon in the solar system is inside the orbit of Mercury, through planetary accumulation from the condensed material to be found there. This explains the anomalous large eccentricity of the orbit of Mercury.