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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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Tables of maximum likelihood estimating functions for singly truncated and singly censored samples from normal distribution
Testing for normality with Kolmogoroff-Smirnoff test
Improved shock normals obtained from combined magnetic field and plasma data from spacecraft
He I line profiles in normal B star spectra
Model sampling or Monte Carlo applied to normal shock, giving temperature and density profiles for Mach 10 shock
Indirect methods of trajectory optimization, improving convergence through normalization of state data and Lagrange multipliers
Fourier spectrum of chopped bivariate normal intensity distribution with coefficients calculated numerically by computer, verifying by chopped laser beam signal analysis
Dietary protein and yeast RNA levels effect on ur acid metabolism in normal man
Normal and unconstrained vacuum-deposited Permalloy films composition dependence of magnetization-induced uniaxial anisotropy, noting agreement with magnetostrictive constraint theory
Normalized multidimensional Newton-Raphson method eliminating initial guess, using two- transformation technique
Practical stability of highly eccentric orbits quasi-normal to ecliptic, discussing lunar effects on orbital lifetime
Coupled supersonic inlet-engine control using overboard bypass doors and engine speed to control normal shock position
Loads due to air and helium jets impinging normal to flat plate for near vacuum and sea level ambient pressures
Ultrasonic attenuation and velocity measurements in normal and superconducting states of niobium
Effect of injectant molecular weight on mixing of normal jet in Mach 4 airstream - tables and graphs
Combustion properties of Teflon insulated wires in supercritical oxygen at normal and zero gravities
Mass matrix and resonant frequencies for generating equivalent spring-mass models for normal modes of structural subsystem
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected normal to supersonic airstreams