A SOLUTION FOR THE NONEQUILIBRIUM FLAT-PLATE BOUNDARY LAYER
Atom concentration in, and heat transfer from, a diatomic gas that is being dissociated by the heat of viscous dissipation in a flat plate boundary layer
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Atom concentration in, and heat transfer from, a diatomic gas that is being dissociated by the heat of viscous dissipation in a flat plate boundary layer
Damping factor from flat annular ring baffles to prevent excessive propellant motion in space vehicle propellant tanks
Flutter of flat rectangular panels based on three-dimensional supersonic potential flow
An analysis is presented for obtaining two-dimensional temperature profiles and heat transfer in a radiation-absorbing gray gas of uniform absorptivity under the combined influence of thermal radiation, conduction, and gas flow. The gas is enclosed in a channel of infinite width and finite length formed by two semi-infinite parallel flat plates. These plates are black emitting surfaces, and the ends of the channel are formed by porous black surfaces through which the gas can flow into or out of the channel. These porous black end surfaces are used to simulate the radiation environment external to the channel. First, results are obtained for heat transfer between the plates in the absence of both conduction and flow. These results are found to be in good agreement with those obtained for the same conditions by previous workers. Results are then presented for heat transfer between the plates for the case of a radiating and conducting, but stagnant, gas separating the plates. The effects of the interactions between radiation and conduction are discussed. It was found that the heat transfer for combined radiation and conduction in an absorbing gas is slightly greater than the sum for each process taken separately. Finally, results are given for heat transfer from the plates to a flowing, radiating gas in the absence of conduction. The two plates are at the same temperature, and the gas enters the channel with uniform velocity and temperature. The results obtained for this case indicate that the heat transferred to the flowing gas from the constant temperature surfaces goes through a maximum as the absorptivity of the gas increases. This is in qualitative agreement with earlier results obtained by other investigators. All the results are presented in terms of dimensionless parameters, for the sake of generality, and the derivation of the dimensionless parameters, which are indicative of the effects of conduction and flow is presented.
Flutter characteristics of curved and flat sandwich panels subjected to supersonic flow
Aerothermic characteristics of flat jet evolving in presence of wall
Membrane analysis of very thin pressurized spheroid shells composed of flat gores - application to Echo II satellite
Supersonic flutter of thermally stressed flat panel with uniform edge loads
Chemical reacting unsteady boundary layer analysis on vaporizing flat plate including compressibility, flame boundary and stagnation point behavior
Flat plate solar thermoelectric generator for near-Earth orbits discussing theory, design, fabrication and testing
Flat plate solar thermoelectric generator design for matched-load condition
Flat plate solar thermoelectric generator panels for near-Earth orbit, discussing design and fabrication
Bismuth telluride base and thermoelectric bond developed for flat plate solar thermoelectric generator
Piezoelectric accelerometer uses a viscous damping technique to achieve a flat frequency response over a wide frequency range in high acoustic environments. This eliminates the electrical overload on associated electronics and loss of useful data caused by oscillations of the accelerometer.
Center-tap push-pull transformer with toroidal core helically wound with a single coaxial cable creates a high frequency wideband transformer. This transformer has a high-turn ratio, a high coupling coefficient, and a flat broadband response.
Unit-mass system of derivation of equations determines the deflection, slope, and moments for thin, flat, circular plates subjected to either a uniform or a symmetrical variable load. The derived equations are computed, organized in tabular form, and graphically depicted.
Method to coat the edges of flat ribbon wire is devised by using enamel with modified flow properties due to addition of 2 to 4 percent silicon. Conventional coating procedes several edge coatings to minimize oxidation and additional conventional coats are applied after edge coating to build up thickness.
Maximum lift-drag ratios for slender flat-top homothetic bodies flying at hypersonic speeds