Electric fields from a horizontal electric dipole situated above a layered lunar half-space Final report
Electric fields from horizontal electric dipole situated above layered lunar half space
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Electric fields from horizontal electric dipole situated above layered lunar half space
Mathematical model for vestibular adaptation to horizontal rotation
Gravity and size effects on film boiling from horizontal cylinders, recommending formulas for wavelength and minimum heat flux predictions
Horizontal branch and red giant stars ratio estimated in globular clusters for He abundance
Two dimensional natural convection boundary layer on finite isothermal horizontal plate, examining upward facing cold plate and downward facing hot plate
Initial horizontal branch metal poor star models, examining opacities, luminosity and cluster ages of RR Lyrae stars
Horizontal branch stars evolution based on mass distributions from comparison with giant branch, investigating evolutionary track characteristics during core helium burning
Stellar spectra above horizontal branch in globular clusters, discussing stellar evolution, composition and structure
Peak pool boiling heat flux on horizontal cylinders, describing interactions of gravity and heater size effects
Development and characteristics of translating horizontal tail assembly for supersonic aircraft
Cryostat for use with horizontal fatigue testing machines at low temperatures
Feasibility of boron-epoxy reinforced aluminum alloy for horizontal stabilizer structure of DC 8 aircraft and recommendations for demonstration program
Low speed wind tunnel test on effects of horizontal tail geometry on longitudinal stability of orbiter shuttle
A static stress analysis and a dynamic modal analysis of the horizontal stabilizer of the F-14A aircraft has been conducted at the Naval Air Development Center employing the NASTRAN program. The structural model contains 1518 elements including bars, rods, shear panels and orthotropic and isotropic membrane elements with 1357 degrees of freedom. Static deflection and stresses, including thermal stresses, under maximum load at room and at elevated temperatures are calculated and results are in good agreement with experimental data. Through application of "Guyan Reduction" the number of degrees of freedom used in the dynamic analysis is reduced to 137 . The frequencies and mode shapes for the first two modes are obtained .
Spicule horizontal component motion from H alpha spectra movies with slit tangential to solar limb
Horizontal cylindrical heaters heat transfer to pool boiling Hg at heat fluxes up to burnout
Horizontal clinostat rotation rate for optimal and acceptable weightlessness simulation in plants, comparing with wheat seedlings growth in Biosatellite 2
Optimum automatic flight control techniques in horizontal guidance of aircraft at terminal