Space related biological and instrumentation studies Annual report, Mar. 1967 - Mar. 1968
Loop antennas for magnetic induction telemeters, and brain temperature probe design
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Loop antennas for magnetic induction telemeters, and brain temperature probe design
Magnetization critical level derived for instability onset for ferromagnetic fluid having nonlinear relation with magnetic induction
Shorted coil of bifilar wound relay to suppress inductive transient voltage, discussing transient response differential equation form of relay model and computer solution
Induction plasma device of continuous operation to simulate NASA designed gas core space propulsion reactor
Neutron flux per unit energy induced in atmosphere by solar neutrons computed as function of atmospheric depth compared to cosmic ray induction
Lunar interior thermal regime measurement method based on dynamo induction of electric field on planetary scale by solar wind
Generation of intense sonic and ultrasonic power in the weld zone, close to the puddle, reduces the porosity and refinement of the grain. The ac induction brazing power supply is modified with long cables for deliberate addition of resistance to that circuit. The concept is extensible to the molding of metals and plastics.
The objective of the effort described in this report was to determine the structural durability of a full-scale advanced annular turbojet combustor using ASTM A-1 type fuel and operating at conditions typical of advanced supersonic aircraft. A full-scale annular combustor of the ram-induction type was fabricated and subjected to a 325-hour cyclic endurance test at conditions representative of operation in a Mach 3.0 aircraft. The combustor exhibited extensive cracking and scoop burning at the end of the test program. But these defects had no appreciable effect on combustor performance, as performance remained at a high level throughout the endurance program. Most performance goals were achieved with pressure loss values near 6% and 8%, and temperature rise variation ratio (deltaTVR) values near 1.25 and l.22 at takeoff and cruise conditions, respectively. Combustion efficiencies approached l004 and the exit radial temperature profiles were approximately as desired.
Wave motion nonsteadyness influence on detonation front thickness using quasi-steady kinetic model of induction process, discussing agreement with experimental observations
Induction plasma device of continuous operation to simulate NASA designed gas core space propulsion reactor
Recording head has standard ferrite core directly coated with a thin film of a magnetic alloy composed of aluminum, iron, and silicon. Coated head has a lifespan from five to ten times longer than that of conventional heads and shows superior inductance characteristics and frequency response.
Resistance-capacitance RC filter coupled to a high input impedance receiver preamplifier provides signal isolation from an RF transmitter. High isolation is achieved by minimizing the inductive impedance to ground and using the distributed capacitance of the filter components.
Feasibility and engineering studies on inverter-motor systems using alternating current induction type motors and quasi-square wave output inverters
Diffused diaphragm pressure sensors in impact probes used in wind tunnel tests of dynamic response of supersonic air induction systems
Molecular dipole moments-electric field interaction induction of cholesteric liquid crystal transition to nematic phase
Pinched plasma reversed current induction due to relativistic electron beam injection
Gas-core nuclear rocket engine simulation by induction coupled plasma torch, determining gas flow patterns
Lithium-like line spectra in Mg, Al and Si observed with grazing incidence spectrometer and low inductance microfarad spark source