Fabrication of high aspect ratio lithographic optical baffles
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Reyna, Robert↗
SEARCH · Engineering Papers
Results for “aspect ratio”
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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Optimization of Copper Electrodeposition in High Aspect Ratio Through Silicon Vias
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McDow, Jessica↗
The Significance of Aspect Ratio in UHF Carbon Nanotube Composite Absorbers
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Padgett, Andrew Scott [Sandia National Laboratorie↗
High aspect ratio structures for meta-surface optics
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Burckel, David Bruce↗
Metal-assisted Chemical Etching of High Aspect Ratio Features in Silicon
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Arrington, Christian Lew [Sandia National Laborato↗
High aspect ratio structures enabled by backside illumination of SU-8
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Burckel, David Bruce [Sandia National Laboratories↗
Neoclassical transport in strong gradient regions of large aspect ratio tokamaks
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neoclassical transport↗
Global gyrokinetic study of shaping effects on electromagnetic modes at NSTX aspect ratio with ad hoc parallel magnetic perturbation effects
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Gyrokinetic simulations↗
Decretion disc size in Be/X-ray binaries depends upon the disc aspect ratio
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Rebecca G Martin↗
EXPERIMENTAL AND THEORETICAL STUDIES OF THE EFFECTS OF CAMBER AND TWIST ON THE AERODYNAMIC CHARACTERISTICS OF PARAWINGS HAVING NOMINAL ASPECT RATIOS OF 3 AND 6
Effects of camber and twist on aerodynamic characteristics of parawings
AERODYNAMIC CHARACTERISTICS↗
EFFECTS OF WING VERTICAL LOCATION ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING
Effects of wing vertical location on stability and control of canard aircraft at supersonic speeds
AIRCRAFT CONTROL↗
Large-scale wind-tunnel tests of an airplane model with an unswept tilt wing of aspect ratio of 5.5, and with various stall control devices
Wind-tunnel stability tests of tilt-wing vtol aircraft
WIND TUNNEL STABILITY TEST↗
Longitudinal aerodynamic characteristics of a 1/30-scale subsonic canard-airplane model having a wing with an aspect ratio of 3.6 at mach numbers from 0.30 to 0.98
Wind tunnel aerodynamic characteristics of subsonic nuclear powered canard aircraft model
NUCLEAR AIRCRAFT↗
A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
Effects of conical camber for triangular wing- body-tail combinations on aerodynamic characteristics
WING BODY↗
Wind-tunnel investigation of the flight characteristics of a model of an aspect- ratio-6 conical-parawing utility vehicle
Wind tunnel studies of flight characteristics of model parawing utility vehicle
FLIGHT CHARACTERISTICS↗
Large-scale wind-tunnel investigation of an airplane model with a tilt wing of aspect ratio 8.4, and four propellers, in the presence of a ground plane
Aerodynamic characteristics of large-scale model of tilt-wing V/STOL aircraft
Deckert, W. H.↗
Thick high aspect ratio wing, part 2
Transonic flutter and buffeting for elastic wind tunnel models of straight wing proposed for space shuttles
Erickson, L. L.↗
Stability and control characteristics of a large scale deflected slipsteam STOL model with a wing of 5.7 aspect ratio
Wind tunnel tests of stability and control characteristics of large scale model representative of propeller-driven STOL transport aircraft
Page, V. R.↗