XVI International Congress of Zoology. Volume 5 - an Account of the Congress
Planning, organization, and proceedings of International Congress of Zoology
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Planning, organization, and proceedings of International Congress of Zoology
Elastic equilibrium in isotropic plate in stationary thermal field, and bending due to temperature stresses
Apollo thermal control systems and concepts, discussing self-shadowing
Light pressure effect on orbital trajectories of space vehicle interorbital flights
Thermal unsteady state effect on coefficient of convective heat transfer during flow round spherical bodies at small Reynolds numbers
Hydrodynamic equations for calculating nonisentropic nonequilibrium gas flow through nozzle induced by friction and heat exchange
Height distribution analysis for kinetic molecular ionization-recombination processes in F 2 region during solar activities
Plane stress analysis using Fourier series of edge stiffened isotropic or orthotropic elastic rectangular plate subjected to prescribed temperature distribution and boundary loads
Activities and operation of New England Research Application Center as information dissemination source
Apollo thermal control systems and concepts, discussing self shadowing
Theoretical shape of magnetosphere boundary considering inclination of geomagnetic dipole and nondipole part of geomagnetic field
EXEC 8 modified multiprogramming system to log core time and central processing unit
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Triatomic hydrogen ion role in solar photosphere opacity implied from limb darkening and specific intensity data
Computer program for determining manpower costs for full time, part time, and contractor personnel is discussed. Twelve different tables resulting from computer output are described. Program is written in FORTRAN 4 for IBM 360/65 computer.
A method has previously been developed to satisfy terminal rendezvous and intermediate timing constraints for planetary missions involving orbital operations. The method uses impulse factoring in which a two-impulse transfer is divided into three or four impulses which add one or two intermediate orbits. The periods of the intermediate orbits and the number of revolutions in each orbit are varied to satisfy timing constraints. Techniques are developed to retarget the orbital transfer in the presence of orbit-determination and maneuver-execution errors. Sample results indicate that the nominal transfer can be retargeted with little change in either the magnitude (Delta V) or location of the individual impulses. Additonally, the total Delta V required for the retargeted transfer is little different from that required for the nominal transfer. A digital computer program developed to implement the techniques is described.
To retain separability in the Vinti theory of earth satellite motion when a nonconservative force such as air drag is considered, a set of variational equations for the orbital elements are introduced, and expressed as functions of the transverse, radial, and normal components of the nonconservative forces acting on the system. In this approach, the Hamiltonian is preserved in form, and remains the total energy, but the initial or boundary conditions and hence the Jacobi constants of the motion advance with time through the variational equations. In particular, the atmospheric density profile is written as a fitted exponential function of the eccentric anomaly, which adheres to tabular data at all altitudes and simultaneously reduced the variational equations to indefinite integrals with closed form evaluations. The values of the limits for any arbitrary time interval are obtained from the Vinti program.
Usually it is expensive to obtain suitable damping coefficients for exterior and interior walls made up of light materials. Hence, acoustic protection problems must be tackled in parallel with the design and introduction of new types of elements. A comparison of classical solutions shows that interior separating walls raise the most difficult problems. In order to reduce building costs it is necessary to make a careful study of architectural solutions and to provide for wall structures with characteristics that vary with the particular case.