Plasmon energies, derived as a function of ρ and f, are discussed.
Consequently, a simplified regression model for a free hanging panel was derived as a function of those selected parameters.
The analytical behavior of the phase SNR is derived as a function of resonance frequency, T2* and echo time.
The effective dislocation source length is derived as a function of sample size by a statistical analysis and experimental data.
The amount of transformation and the transformation plasticity is derived as a function of the driving force.
Then, an analytical formulation of postbuckling and buckling vibration is derived as a function of the external compressive axial load.
The equivalent Young's modulus, Poisson's ratio, and coefficient of thermal expansion of a material are theoretically derived as a function of temperature.
Infiltration is derived as a function of lithology, lineament density, karstification and drainage density, all of which can be easily extracted from satellite imagery.
Consequently, a first order linear regression equation, or the simplified CRCP model, was derived as a function of the major single parameters and two-factor interactions.
As a result, much simpler asymptotic closed-form formula for distortion of PPCQ is derived as a function of the support region threshold.
By imposing the balance between required and available power, the endurance expression is derived as a function of airframe features, rotor parameters, and battery capacity.
