Performance of 84 deg flat-plate helical inducer and comparison with performance of similar 78 deg and 80.6 deg inducers
Performance of 84 deg flat plate helical inducer compared with 78 deg and 80.6 deg inducers
HELICAL INDUCER↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Design analysis and general characteristics of flat-plate central-fin-tube sensible-heat space radiators
Design analysis and general characteristics of flat plate central fin-tube sensible-heat space radiators under thermodynamic and fluid mechanic conditions
FLAT PLATE↗
Local turbulent skin-friction measurements on a flat plate at mach numbers from 2.5 to 4.5 and reynolds numbers up to 69 x 106
Supersonic wind tunnel tests of turbulent skin friction on flat plate at very high Reynolds number
REYNOLDS NUMBER↗
On free vibrations of eccentrically stiffened cylindrical shells and flat plates
Free vibrations of eccentrically stiffened cylindrical shells and flat plates
FLAT PLATE↗
Measurements of nonequilibrium effects in air on wedge-flat-plate afterbody pressures
Heat transfer properties of wedged, flat plate in high temperature air - thermochemical nonequilibrium effects
FLAT PLATE↗
The contact of certain elastic shells with rigid flat surfaces Technical report no. 3
Stress and shear deformation analysis for simple symmetric elastic shells in contact with rigid flat surface
ELASTIC SHELL↗
Flat conductor wiring systems for federal and commercial applications
Flat conductor wiring system design, materials, production, characteristics, and applications
FLAT LAYER↗
Film boiling heat transfer to water drops on a flat plate
Evaporation rates and heat transfer coefficients for water drops supported by own superheated vapor over flat hot plate
FILM BOILING↗
Laminar slip flow in a flat duct or a round tube with uniform wall heat transfer
Low density phenomena effect on heat transfer for laminar flow in flat duct or circular tube with uniform wall heat flux
FLAT SURFACE↗
One-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
One-dimensional approach to maximum lift-drag ratio of slender, flat-top, affine wing at hypersonic speeds
FLAT SURFACE↗
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Two-dimensional approach to maximum lift-drag ratio of slender, flat-top, wing at hypersonic speeds
FLAT SURFACE↗
Further investigation of effect of air injection through slots and porous surfaces on flat-plate turbulent skin friction at Mach 3
Supersonic flat plate skin friction reduction by air injection into turbulent boundary layer
GAS INJECTION↗
A study of the pressure, heat transfer, and skin friction on sharp and blunt flat plates at Mach 6.8
Pressure, heat transfer, and skin friction studies on sharp and blunt flat plates at hypersonic speeds
FLAT PLATE↗
Analysis, design and development of a flat plate solar thermoelectric energy conversion panel Final report, 12 Jun. - 12 Dec. 1963
Analysis, design, and development of flat plate solar thermoelectric energy conversion panel
FLAT PLATE↗
Analysis, design and development of a flat plate solar thermoelectric energy conversion panel Final report, 17 Apr. - 17 Oct. 1964
Analysis, design, and development of flat plate solar thermoelectric energy conversion panel
FLAT PLATE↗
Analysis of solar thermoelectric flat-plate generators operating in the range of 1.0 to 0.1 astronomical unit
Lead telluride and silicon-germanium panels for solar thermoelectric flat plate generators
LEAD TELLURIDE↗
Pressure distributions on a flat-plate delta wing swept 65 deg at a Mach number of 5.97 at angles of attack from 65 deg to 115 deg and angles of roll from 0 deg to 25 deg at a 90 deg angle of attack
Pressure distributions on flat plate delta wing swept 65 deg at hypersonic speeds at angles of attack from 65 deg to 115 deg and angles of roll from 0 deg to 25 deg at 90 deg angle of attack
ANGLE OF ATTACK↗
Heat-transfer and pressure distributions on a flat-face rounded-corner body of revolution with and without a flap at a Mach number of 8
Heat transfer and pressure distributions on flat face rounded-corner body of revolution with and without flap control at hypersonic speeds and angles of attack from 0 deg to 45 deg
FLAT SURFACE↗