Two-component Magnetic Field along the Line of Sight to the Perseus Molecular Cloud: Contribution of the Foreground Taurus Molecular Cloud
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Yasuo Doi↗
SEARCH · Engineering Papers
Results for “hull”
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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Multipoint Observations of Dispersive Scale Alfvénic Field‐Line Resonances Associated With Substorm Auroral Beads
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Arthur J. Hull↗
Reply to Comment by Nishimura Et Al.
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F. S. Mozer↗
A Survey of Dense Low Energy Ions in Earth's Outer Magnetosphere: Relation to Solar Wind Dynamic Pressure, IMF, and Magnetospheric Activity
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Arthur J. Hull↗
The JCMT BISTRO Survey: multiwavelength polarimetry of bright regions in NGC 2071 in the far-infrared/submillimetre range, with POL-2 and HAWC+
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Lapo Fanciullo↗
Functional relation between stimulus intensity and photically evoked cerebral responses in man.
Stimulus intensity and photically evoked cerebral response as possible objective index of brightness perception for man
BRIGHTNESS DISCRIMINATION↗
The generation of random interval schedules.
Generation of reinforced random interval schedules, using electronic precision probability unit consisting of multibrator and clock
SIGNAL ANALYZER↗
Maximum lift-to-drag ratios of a slender, flat-top, hypersonic bodies, part 1
Maximum lift-drag ratios for slender flat-top homothetic bodies flying at hypersonic speeds
HYPERSONIC SPEED↗
Three-dimensional, lifting wings of minimum drag in hypersonic flow
Three-dimensional lifting wings of minimum drag in hypersonic flow
SLENDER WING↗
Three-dimensional Wings of Maximum Lift-to- Drag Ratio in Hypersonic Flow
Optimizing lift-to-drag ratio of slender, flat-top wing of given planform in hypersonic flow by using variational calculus methods
LIFT-DRAG RATIO↗
Feasibility study of an optical radiometer for determining the composition of the Mars atmosphere from shock layer radiation during entry, volume II Final report
Optical radiometer feasibility study for determining composition of Mars atmosphere from shock layer radiation during entry - instrumentation
INSTRUMENTATION↗
Two-dimensional, Lifting Wings of Minimum Drag in Hypersonic Flow
Two-dimensional lifting wings of minimum drag in hypersonic flow
SLENDER WING↗
Two-dimensional Wings of Maximum Lift-to-drag Ratio in Hypersonic Flow
Two-dimensional wings of maximum lift-drag ratio in hypersonic flow
HYPERSONIC FLOW↗
Maximum Lift-to-drag Ratio of a Slender, Flat-top, Hypersonic Body
Maximum lift-drag ratio of slender, flat top, hypersonic body assuming modified Newtonian pressure distribution and constant surface averaged skin friction coefficient
SLENDER BODY↗
Two-dimensional, hypersonic wings of maximum lift-to-drag ratio.
Slender two-dimensional wing lift-drag ratio at hypersonic speed maximized, assuming modified pressure coefficient
PRESSURE COEFFICIENT↗
Three-dimensional, hypersonic wings of maximum lift-to-drag ratio.
Three-dimensional slender wings of maximum lift/ drag ratio in hypersonic flow studied by variational calculus under several lift and volume conditions
THREE-DIMENSIONAL FLOW↗
Maximum lift-to-drag ratio of a slender, flat-top, hypersonic body.
Lift-drag ratio attainable by slender flat-top body at supersonic speeds, considering Newtonian pressure distribution and constant skin friction
NEWTONIAN FLUID↗