FORTRAN subprograms for complete elliptic integrals
FORTRAN subroutines for complete elliptic integrals
Zonis, F. I.↗
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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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Optimisation of aircraft performance and mission completion through research on the pilot and aircraft as an overall system.
Optimization of aircraft performance, pilot performance and mission completion
Beeler, De E.↗
The axisymmetric response of a complete cylindrical shell to shock loads.
Axisymmetric dynamic response of complete cylindrical shell to shock loads using bending theory of thin shells
Stadler, W.↗
An axiomatic explanation of complete self- reproduction.
Axiomatic explanation of complete self reproduction, noting logical mathematical biological reasoning and evolution theories
Loefgren, L.↗
Nonsymmetric modes of complete spherical shells.
Complete spherical shells nonsymmetric vibrations frequencies and mode shapes calculated by matrix method
Gormley, J. F.↗
Feasibility of manual completion of a LOI burn. Volume 1 - IMU drift about the pitch axis
Manual completion of lunar orbit insertion burn with inertial measuring unit drifting about pitch axis
Treadway, A. H.↗
Feasibility of manual completion of a LOI burn. Volume 2 - BMAG drift about the pitch axis. Project Apollo
Feasibility of manual completion of LOI burn with body mounted attitude gyro drifting about pitch axis
Treadway, A. H.↗
On a criterion for determining the complete continuity of Urysohn's integral operator
Nonlinear operator for determining complete continuity when kernel is function of variables
Nurekenov, T.↗
Computer program: Jet 3 to calculate the large elastic plastic dynamically induced deformations of free and restrained, partial and/or complete structural rings
A user-oriented FORTRAN 4 computer program, called JET 3, is presented. The JET 3 program, which employs the spatial finite-element and timewise finite-difference method, can be used to predict the large two-dimensional elastic-plastic transient Kirchhoff-type deformations of a complete or partial structural ring, with various support conditions and restraints, subjected to a variety of initial velocity distributions and externally-applied transient forcing functions. The geometric shapes of the structural ring can be circular or arbitrarily curved and with variable thickness. Strain-hardening and strain-rate effects of the material are taken into account.
Wu, R. W.↗
Concerns of the Institute of Transport Study and Research for reducing the sound level inside completely repaired buses
Sound level measurements on noise sources on buses are used to observe the effects of attenuating acoustic pressure levels inside the bus by sound-proofing during complete repair. A spectral analysis of the sound level as a function of motor speed, bus speed along the road, and the category of the road is reported.
Groza, A.↗
Vibration analysis of a completely free elliptical plate
The Ritz method is applied to the variation analysis of a completely free elliptical plate as an efficient alternative to a procedure using a truncated series of regular and modified Mathieu functions. It is shown that a solution as accurate as desired can be obtained with the Ritz method in solving thin plate vibration problems with difficult geometries.
Beres, D. P.↗
Wave propagation in a random medium - A complete set of the moment equations with different wavenumbers
The propagation of waves in a random medium is studied in the 'quasi-optics' and the 'Markov random process' approximations. Under these assumptions, a Fokker-Planck equation satisfied by the characteristic functional of the random wave field is derived. A complete set of moment equations with different transverse coordinates and different wave numbers is then obtained from the Fokker-Planck equation of the characteristic functional. The application of those results to the pulse smearing of the pulsar signal and the frequency correlation function of the wave intensity in interstellar scintillation is briefly discussed.
Lee, L. C.↗
Transient and steady-state velocity of domain walls for a complete range of drive fields
Approximate analytic solutions for transient and steady-state 180 deg domain wall motion in bulk magnetic material are obtained from the dynamic torque equations with a Gilbert damping term. The results for the Walker region in which the transient solution approaches the familiar Walker steady-state solution are presented in a slightly new form for completeness. An analytic solution corresponding to larger drive fields predicts an oscillatory motion with an average value which decreases with drive field for reasonable values of the damping parameter. These results agree with those obtained by a computer solution of the torque equation and those obtained with the assumption of a very large anisotropy field.
Bourne, H. C., Jr.↗
Small parametric model of the precomputation of meteorological fields on the basis of complete equations and its energetic analogs
A small parametric, nonadiabatic model for precomputation of meteorological fields on the basis of complete equations, along with its energetic analogs is described. The model incorporates integral characteristics of the components of the wind speed and the analogous functions of the total fluxes of the ocean, and uses a Cartesian isobaric system of coordinates.
Borisenkov, Y. P.↗
Transient and steady-state velocity of domain walls for a complete range of drive fields
Approximate analytic solutions for transient and steady-state 180 deg domain-wall motion in bulk magnetic material are obtained from the dynamic torque equations with a Gilbert damping term. The results for the Walker region in which the transient solution approaches the familiar Walker steady-state solution are presented in a slightly new form for completeness. An analytic solution corresponding to larger drive fields predicts an oscillatory motion with an average value of the velocity which decreases with drive field for reasonable values of the damping parameter. These results agree with those obtained by others from a computer solution of the torque equation and those obtained by others with the assumption of a very large anisotropy field.
Bourne, H. C., Jr.↗
Necessary and sufficient conditions for the complete controllability and observability of systems in series using the coprime factorization of a rational matrix
The series connection of two linear time-invariant systems that have minimal state space system descriptions is considered. From these descriptions, strict-system-equivalent polynomial matrix system descriptions in the manner of Rosenbrock are derived. They are based on the factorization of the transfer matrix of the subsystems as a ratio of two right or left coprime polynomial matrices. They give rise to a simple polynomial matrix system description of the tandem connection. Theorem 1 states that for the complete controllability and observability of the state space system description of the series connection, it is necessary and sufficient that certain 'denominator' and 'numerator' groups are coprime. Consequences for feedback systems are drawn in Corollary 1. The role of pole-zero cancellations is explained by Lemma 3 and Corollaires 2 and 3.
Callier, F. M.↗
A complete model of turbulence
A set of constitutive equations suitable for a priori computation of turbulent shear flows has been developed. Since no properties of a given turbulent flow need be known in advance in order to obtain a solution, the equations comprise a complete model of turbulence. Perturbation analysis shows that the model predicts a composite five-layer structure for an incompressible turbulent boundary layer, viz, a defect layer, a law-of-the-wall layer, a viscous sublayer, a near-surface roughness layer, and a viscous superlayer at the boundary-layer edge. Analysis of the defect layer demonstrates the key improvement of the model over its predecessor, the Saffman-Wilcox two-equation model of turbulence. Examination of model-predicted sublayer structure yields model-parameter boundary conditions appropriate for surfaces with roughness and mass injection. Results of numerical computations of compressible and incompressible equilibrium boundary layers show that, for such flows, the model is as accurate as mixing-length theory. Applications to transitional boundary layers and to nonequilibrium relaxation of a boundary layer passing from a rough to a smooth surface indicate that the model's applicability extends far beyond that of mixing-length theory's.
Wilcox, D. C.↗
Concepts for the design of a completely active helicopter isolation system using output vector feedback
The theory of output vector feedback (a few measured quantities) is used to derive completely active oscillation isolation functions for helicopters. These feedback controller concepts are tested with various versions of the BO 105 helicopter and their performance is demonstrated. A compensation of the vibrational excitations from the rotor and harmonics of the number of blades are considered. There is also a fast and automatic trim function for maneuvers.
Schulz, G.↗