Comparative studies of some simple viscoelastic theories
Comparative studies of some simple viscoelastic theories
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Comparative studies of some simple viscoelastic theories
Momentum integral method treating magnetohydrodynamic and simple hydrodynamic entrance flows
Simple equations for temperature distributions in radiating gray gases
Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach numbers of 3 and 6
Dipole antenna current distribution, deriving simple, accurate formula for infinite, semiinfinite and finite cases
Simple antenna with good circular polarization over wide space sector, showing geometry, normalized orthogonal field distributions and beamwidth range, considering slot combinations
Lyman alpha radiation from electron collisions with simple H-containing molecules, finding dissociative excitation cross section role
Fatigue-crack growth under simple variable amplitude loading in aluminum alloys
Drift of noninteracting charged particles in simple geomagnetic field
Modifications to Fourier law of heat conduction through use of simple collision model
Approximations to Bayes estimate for quantal assay with simple exponential tolerance distribution
Acetylcholinesterase and simple esterases distribution in squirrel monkey brain, examining activity in neuropil and postrema area neurons
Prism plus image amplifier panel provides visual image of many infrared spectral lines from carbon arc impregnated with metal compound. Different metal compounds generate various desired spectra. Panel also aligns and focuses simple spectroscopes for detecting spectral lines inside and outside visible region.
Examination of simple coordinate transformations in Z-plane and W-plane for root locus analysis of sampled data systems
Measuring Auger spectra of simple gaseous molecules
Definition and implementation of simple LR/k/ context free grammars
Wind tunnel investigation of lift-induced sonic boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63
Simple integral method for calculating real gas turbulent boundary layers with variable edge entropy and flight calculations showing effect of nose bluntness at 6.09 km/sec