Chrysler improved numerical differencing analyzer for 3rd generation computers
FORTRAN computer program for solution of thermal analog models by Univac 1108 computer
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FORTRAN computer program for solution of thermal analog models by Univac 1108 computer
Joyce-Loebl microdensitometer-isodensitracer for infrared film density analysis
Study of mammalian blood to determine glucose levels and the effects of polycythemia and hyperoxia
Aerodynamic stability of helicopter rotor in forward flight
Satellite measurements of suprathermal electrons at conjugate sunrise, indicating photoelectron escape from production level and movement along geomagnetic lines into conjugate ionosphere
Venus carbon dioxide spectral band analysis methods, discussing spectral lines and rotational temperatures obtained
Electronic system /MIRACLE 2/ places frequency and gas flow rate of the respiratory process within a common frame of reference to render them comparable and compatible with ''real clock time.'' Numerous measurements are accomplished accurately on a strict one-minute half-minute, breath-by-breath, or other period basis.
Micrometeoroid mass, velocity, and composition from impact flash signature by spectroscopic analysis
Analysis of secondary flow effects in propeller and rotor boundary layers
Method of characteristics for calculating oblique shock wave interaction with turbulent boundary layer
Formation, growth and permeability of pressurant gases and propellant vapors through laminated bladder structures
Computer program for determining performance and system requirements of electrically propelled spacecraft missions
Determining compatible internal states of inverse automation by analysis of original automation
Design and modification of pyrolysis, gas chromatograph, double focusing mass spectrometer and addition of heated ion source for Martian life detection
Linear acceleration effects on semicircular canals in elasmobranch fishes
Permeation of high density gases and propellant vapors through laminated Teflon expulsion bladders
Three dimensional latching dynamics and loads induced during Apollo spacecraft docking, using linear stiffness or flexibility matrices for structural elasticity
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