Secondary particle spectra from the interaction of 30- to 340-Mev protons on complex nuclei - Experimental data and comparison with theory.
Neutron and proton spectra anomalies from proton- nuclei interactions in 100 Mev region
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Neutron and proton spectra anomalies from proton- nuclei interactions in 100 Mev region
Temperature distributions measured on top surface of cylindrical specimens for determining effective thermal conductivity of solid and porous tungsten in vacuum and hydrogen
Dissociation relaxation times of carbon dioxide
Cosmos and Explorer satellite data used to reject hypothesis of terrestrial meteoroid and dust clouds
Performance data for high tip speed compressor rotor operated with radial and inlet airflow distortions
Data analysis on filament reinforced metal matrix composites
Compressible hypersonic turbulent boundary layers solution by finite difference method, relating mixing length to velocity profile shape factor
Dynamic test analysis on modal damping forces of Saturn 5 Apollo vehicle
Numerical solution of compressible laminar, transitional, and turbulent boundary layer equations
Compressible hypersonic turbulent boundary layers solution by finite difference method, relating mixing length to velocity profile shape factor
High speed data transmission system for remote data acquisition using data bus
Calculation of electron concentration for blunt nose at orbital speeds by use of pure air nonequilibrium chemistry throughout flow field and for same flow field with alkali contaminants
Numerical solution of flow equations for laminar, transitional, and turbulent compressible boundary layers for planar or axisymmetric flows
Performance tests of compressor seals and stator pivot seals used with air breathing propulsion systems - Part 2
Biophysical model of life origin on earth using primordial gas-small organic molecule- macromolecule-protocell transformations
A program is described for obtaining resonant frequencies, modal amplitudes, and damping of a structure from a sinusoidal force-controlled vibration test. Presented are the theoretical basis for the analysis (the Kennedy-Pancu method), recommendations for a test procedure based on experience with several earlier test programs, and an outline of the data analysis technique. Although the program was developed for structural vibration problems, variations for processing any sinusoidal data are available.
Brief review of the operational principle and capability of the high-Reynolds-number wind tunnel developed over the last few years. Its test medium is stored in a Ludwieg tube and held there by means of a diaphragm. When the diaphragm is broken, a rearward-facing centered rarefaction fan propagates upstream through the test section and nozzle into the supply tube, and the useful run time is bounded by the reflected rarefaction wave and the starting shock wave caused by choking at the nozzle. The operating problems center around the ability of model and sting support systems to withstand the loads and to meet the instrumentation requirements. Evaluation tests have shown that satisfactory force and moment measurements can be obtained in this facility.
A computer program previously developed to analyze three-dimensional supersonic nozzles by the method of characteristics has been modified to study less restrictive nozzle geometries and nonuniform inlet conditions. An example indicates that a one-dimensional calculation that uses an averaged initial profile may be significantly in error. A comparison between the analysis and the data from a three-dimensional experiment shows generally good agreement between the two.