Cell-cluster development for the pair distribution function - Application to rigid disks at hight density.
Molecular pair distribution function in perfect crystalline solids, using method based on cell cluster theory
MOLECULAR STRUCTURE↗
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Dexterity enhancement in microsurgery using telemicro-robotics
The presentation will focus on finding the spectrum of dexterity performance while performing microsurgery in various specialties. It will be noted that individuals vary markedly in their performance in the position, velocity, stability, and force domains. There are surgeons who have a tremor who otherwise move very slowly and carefully while there are other surgeons who apply excessive force, but never have a tremor or move excessively fast. There are yet other surgeons who move excessively fast, yet they do not have a tremor. Dexterity enhancement includes position down scaling, tremor filtering, fatigue elimination, and other second-order issues such as confining the work space, velocities, accelerations, or forces. It will be described that the hand's position performance is degraded when it is asked to actuate the tools and that remote actuation alone increases the positioning capabilities. It will be noted that rotary and telescopic functions are far more difficult than writing or engraving-like motions. The safety issues concerning velocities and forces will be discussed and the need for impedance control pointed out. Simplistically, the devices should be made with variable compliance so that they can function rigidly as a robot would or compliantly as a human would, depending on the setting of this parameter. Tool interfaces will be discussed with an emphasis on the overall performance of the position, end effector, and tool as a unit. Space constraints, force, and velocity requirements will be discussed in this section as well. Referencing the coordinate system to pre- or inter-operative imaging systems will be discussed as well as an emphasis on the system architecture.
Charles, Steve↗
Calculation and Compilation of the Unsteady-lift Functions for a Rigid Wing Subjected to Sinusoidal Gusts and to Sinusoidal Sinking Oscillations
The total lift responses to sinusoidal sinking oscillations and to sinusoidal gusts have been calculated, largely from existing information, for wings of various plan forms in subsonic and supersonic flow. For most of the cases considered, closed-form expressions are given and the final results are presented in the form of plots of the square of the modulus of the lift coefficient for wings in a sinusoidally oscillating gust field and in the form of the real and imaginary parts of the lift coefficient for wings undergoing sinusoidal sinking oscillations.
LOADS, GUST - WINGS↗
Pressure correlation for a cylinder in a diffuse sound field.
Surface pressure spatial correlation function for rigid infinitely long cylinder in three- dimensional diffuse sound field
CORRELATION FUNCTION↗
Generic Karman-Rostovstev plate equations in an affine space
The Karman-Rostovstev plate equations are affinely transformed into equations that depend on the generic plate constants generalized rigidity, generalized extensional rigidity, and generalized Poisson ratio associated with the well-known linearized orthotropic plate/slab equations. Furthermore, since the generalized extensional rigidity is a function of generalized rigidity and generalized Poisson ratio only, with generalized Poisson ratio being a weak parameter, the only fundamental constant is generalized rigidity. This means that regardless of what analysis technique is used, the results can be cast in terms of only one strong material parameter (whose range is from zero to one). The affine stretching is performed on the dependent variables as well as the independent variables, so that the dependence of all quantities of interest on generalized rigidity and generalized Poisson ratio are easily calculated (e.g., even auxiliary quantities such as stress, strain, all weighted stress resultants, etc.). Some typical results (static side load response, collapse load limited by rib buckling) are presented by modifying an approximate technique due to Donnell (1976).
Brunelle, E. J.↗
Neutron measurements in near-Earth orbit with COMPTEL
The fast neutron flux in near-Earth orbit has been measured with the COMPTEL instrument on the Compton Gamma Ray Observatory (CGRO). For this measurement one of COMPTEL's seven liquid scintillator modules was used as an uncollimated neutron detector with threshold of 12.8 MeV. The measurements cover a range of 4.8 to 15.5 GV in vertical cutoff rigidity and 3 deg to 177 deg in spacecraft geocenter zenith angle. One of the measurements occurred near the minimum of the deepest Forbush decrease ever observed by ground-level neutron monitors. After correction for solar modulation, the total flux is well fitted by separable functions in rigidity and zenith angle. With the spacecraft pointed near the nadir the flux is consistent with balloon measurements of the atmospheric neutron albedo. The flux varies by about a factor of 4 between the extremes of rigidity and a factor of 2 between the extremes of zenith angle. The effect of the spacecraft mass in shielding the detector from the atmospheric neutron albedo is much more important than its role as a source of additional secondary neutrons. The neutron spectral hardness varies little with rigidity or zenith angle and lies in the range spanned by earlier atmospheric neutron albedo measurements.
Morris, D. J.↗
The enigma of the Uranian satellites' orbital eccentricities
The eccentricity decay times for the Uranian satellites are calculated using recent observations (Brown et al., 1982) of the diameters and orbital elements of the satellites and assuming reasonable dissipation functions and rigidities for icy satellites. For the outer two satellites, Titania and Oberon, the decay times are found to be very long, whereas the inner three satellites, Miranda, Ariel, and Umbriel, have decay times on the order of 10 to the 7th to 10 to the 8th years and have a near-commensurability in their mean motions that cannot force their eccentricities. There are several possible solutions for the lack of resonant forcing: (1) the reported eccentricities are incorrect, and are very nearly zero, (2) the reported mean motions are incorrect, and an exact commensurability exists, (3) the physical properties assumed for the satellites are grossly in error, and (4) the system is evolving rapidly, perhaps from a previous state of higher eccentricity. A new lower bound of about 17,000 on the dissipation function of Uranus is calculated from the mass of Ariel and its proximity to Uranus.
Squyres, S. W.↗
Hard-sphere solid - Pair distribution functions at high density.
High density form of molecular pair distribution function for rigid spheres system, using cell- cluster technique
Larsen, R. D.↗
A dynamical theory of elastic directed curves.
Elastic directed curves dynamic theory, considering Hamilton principle, mass conservation and behavior of action density function under rigid body variations
Desilva, C. N.↗
Electromagnetic power absorber
Device has reflection coefficient of order of few tenths of percent and is designed to maintain isothermal temperature distribution in high-power microwave and laser applications. Rigid tile functions over broad temperature range and serves as blackbody radiometric standard. Tile modules allow assembly of compact and economical custom-design configurations. Epoxy surface of tiles is insulated with styrofoam against environmental changes and is not subject to convective heat loss. Technique also prevents moisture accumulation and serves as infrared radiation shield.
Iwasaki, R.↗
Rigid disks and spheres at high densities - Bounds on the partition function.
Upper and lower bounds on partition functions for finite systems of rigid disks and spheres for high density limit
FACE CENTERED CUBIC /FCC/ CRYSTAL↗
Tunnel model for rigid disks near close packing.
Partition function for tunnel model of rigid disks evaluated in asymptotic limit of reduced volume, including close-packed value of closed systems area
DISK↗
Vibrational spectra and structure of small-ring compounds. XII.
Propylene imine IR and Raman spectra, calculating thermodynamic functions based on rigid rotator harmonic oscillator model
Bush, S. F.↗
Ride comfort control in large flexible aircraft
The problem of ameliorating the discomfort of passengers on a large air transport subject to flight disturbances is examined. The longitudinal dynamics of the aircraft, including effects of body flexing, are developed in terms of linear, constant coefficient differential equations in state variables. A cost functional, penalizing the rigid body displacements and flexure accelerations over the surface of the aircraft is formulated as a quadratic form. The resulting control problem, to minimize the cost subject to the state equation constraints, is of a class whose solutions are well known. The feedback gains for the optimal controller are calculated digitally, and the resulting autopilot is simulated on an analog computer and its performance evaluated.
Warren, M. E.↗
Tidal dissipation, orbital evolution, and the nature of Saturn's inner satellites
Estimates of tidal damping times of the orbital eccentricities of Saturn's inner satellites place constraints on some satellite rigidities and dissipation functions Q. These constraints favor rock-like rather than ice-like properties for Mimas and probably Dione. Photometric and other observational data are consistent with relatively higher densities for these two satellites, but require lower densities for Tethys, Enceladus, and Rhea. This leads to a nonmonotonic density distribution for Saturn's inner satellites, apparently determined by different mass fractions of rocky materials. In spite of the consequences of tidal dissipation for the orbital eccentricity decay and implications for satellite compositions, tidal heating is not an important contributor to the thermal history of any Saturnian satellite.
Peale, S. J.↗
Ulysses high energy particle observation of the effects of recurrent high speed streams
Since June 1992 The Kiel Electron Telescope on board Ulysses measures variations of more than 10% in the fluxes of high energy H and He showing a periodicity of about 27 days, which are coincident with the passage of corotating interaction refios (CIR). At low energies MeV protons are accelerared at the shocks of the CIRs. These effects were observed up to high southern latitudes, where the signature of time of the conference Ulysses will have passed the solar equator and climbed up to 70 deg N at solar distance of 1.7 AU. In this paper we study the intensity variations with latitude as a function of magnetic rigidity.
Droege, W.↗
The Development of a Dynamic Geomagnetic Cutoff Rigidity Model for the International Space Station
We have developed a computer model of geomagnetic vertical cutoffs applicable to the orbit of the International Space Station. This model accounts for the change in geomagnetic cutoff rigidity as a function of geomagnetic activity level. This model was delivered to NASA Johnson Space Center in July 1999 and tested on the Space Radiation Analysis Group DEC-Alpha computer system to ensure that it will properly interface with other software currently used at NASA JSC. The software was designed for ease of being upgraded as other improved models of geomagnetic cutoff as a function of magnetic activity are developed.
Smart, D. F.↗