Analyzation, design, fabrication, and testing of a foil bearing rotor support system Final technical report
Foil journal bearing rotor support system - design and fabrication
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Foil journal bearing rotor support system - design and fabrication
Automatic recording instrument for distribution curves of random electric signals
Combination of point counting and electron microprobe techniques in mineralogical planimetric integration analysis
Optimal gain settings for atmospheric turbulence in 407 Jimsphere wind profiles
Amplitude and wave shape of averaged evoked responses in awake animals including man
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Explore the source record for details and available documents.
Explore the source record for details and available documents.
Explore the source record for details and available documents.
Nephelometer measures aerosol particles in wide concentration and size distribution ranges. It measures the light scattered from the aerosol particles at a controlled sampling rate to ensure laminar flow through the sample tube, and thereby eliminate the need for sheath air.
Digital computer programs determine steady-state performance characteristics of active and passive linear circuits. The ac analysis program solves the basic circuit parameters. The compiler program solves these circuit parameters and in addition provides a more versatile program by allowing the user to perform mathematical and logical operations.
Chronic gamma radiation effects on vestibular apparatus of guinea pigs and role of time factor in radiation reactions of nervous system
Computer program for thermal analyses of complex transient heat transfer problems
Computer tape recording of dynamic data characterized by time varying frequency spectrum
Gas and liquid chromatographic systems for separating and identifying organic compounds - pyrolysis, mass spectrometry, and infrared analytical devices
Optimal gain settings for atmospheric turbulence in 407 atmosphere wind profiles
Computer program performs stability analyses for a wide class of shells without unduly restrictive approximations. The program uses numerical integration, finite difference of finite element techniques to solve with reasonable accuracy almost any buckling problem for shells exhibiting orthotropic behavior.
Computer program formulates geometric description of the wing body configuration, optimizes wing camber shape, determines wing shape for a given pressure distribution, and calculates pressures, forces, and moments on a given configuration. The program consists of geometry definition, transformation, and paneling, and aerodynamics, and flow visualization.