Relationship between crosslink type and mechanical properties
Relationship between crosslinking and mechanical properties of sulfur vulcanizates
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Relationship between crosslinking and mechanical properties of sulfur vulcanizates
Relationship between binocular depth perception and optical distortion in Apollo pressure suit helmets and visors
Determination of time-temperature-vacuum relationships for sterilization of terrestrial spores
Relationships between random and nonrandom probabilities corresponding to instantaneous and identical events
Parametric study of time-temperature-vacuum relationships for terrestrial spore sterilization
Polarization-albedo relationship for selected lunar regions
The problem of predicting the distribution of heat flux in a rocket engine is complicated by a flow field and thermodynamics so perturbed by as yet indescribable combustion effects that it continues to be necessary to utilize a simplified theoretical model against which to compare experimental results in order to gain insight. The most successful model applied to this problem is that of a compressible, turbulent, accelerating boundary layer flow with an arbitrary point of origin, and chemical reaction restricted to equilibrium recombination or diffusion-limited recombination on a catalytic wall. Analysis of this model was not possible without making several assumptions about the nature of the skin friction coefficient relationship and Reynold's analogy in an accelerating boundary layer flow. The paper summarizes the analysis of this model (together with detailed treatment of the special problems of variable properties, chemical reaction, and sources of transport properties), and describes several closed-form equations that have also been developed and applied to the problem. Described are results of several experiments with hot air flow made for the purpose of checking the validity of the assumptions in the boundary layer analysis. Most significant, however, are presentations of sample distributions of local heat flux measured in rocket engines operating with a wide range of conditions, propellants, injectors and sizes. When compared with predictions, these data show the significant range of deviation in heat flux that results from the combustion effects and which precludes a generally accurate prediction theory or correlation equation until the combustion process itself is correlated.
Relationship between instabilities and turbulence in plasma, using spectrum of plasma fluctuations
Radiation effects in man, searching for dose relationships in prodromal syndrome
Mixing function vs time relationship for liquid propellant explosion hazards prediction, noting thermocouple grid for maximum information
Protein and nucleic acid building blocks sequence differences influence on evolutionary relationship of living organisms, comparing fish and mammal globins
Chondritic meteorites initial orbits evolution to earth impact calculated by Monte Carlo method, considering relationships to meteorite sources
Flux magnitude and pitch angle distribution relationship for postsubstorm auroral electrons, noting particle precipitation and acceleration models
Circadian rhythm phase relationships between photoperiodism and heart rate, locomotor activity and deep body temperature /DBT/ in unrestrained monkeys
Thunderstorm turbulence relationship to weather radar echoes from storm penetrations in Oklahoma by instrumented aircraft
Existence limits of cells, isoprenes, genetic systems, E. coli, and cell membranes in intracellular relationships
Relationship between preharvest yield indicators and film densities of aerial infrared film in microexperiments
Relationship between aircraft system performance and pilot ratings