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Los Alamos National Laboratory Floodplain Assessment for the West Road Post and Cable Fencing Project
The National Nuclear Security Administration (NNSA), a semi-autonomous agency within the U.S. Department of Energy (DOE), is proposing to take action at Los Alamos National Laboratory (LANL) to install post and cable or in-kind barriers along West Road at selected locations near the Los Alamos County ice-skating rink in Los Alamos Canyon (Figure 1). The proposed project is intended to improve vehicular and pedestrian safety on West Road by reducing traffic hazards associated with unsafe roadside parking and reduce wildland fire hazards associated with vehicles driving and parking on vegetation. West Road crosses approximately 0.35 miles (mi.) (1,900 feet (ft.)) of the Los Alamos Canyon floodplain at the bottom of Los Alamos Canyon. Project activities within the floodplain include blocking access to the informal roadside parking along either side of West Road in Los Alamos Canyon.
A miniature, directional surface-fence gage
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Experimental investigation of apex fence flaps on delta wings
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Peeking through the picket fence - What astrophysical surprises may be present in the 100-200 A region?
In anticipation of more sensitive EUV and FUV spectroscopic instruments, spectra are simulated including interstellar absorption of solarlike, RS CVn, and flare stars as folded through the instrument parameters of the EUVE, Lyman/FUSE Phase A, and a desirable next-generation spectrometer. Even the relatively insensitive EUVE spectrometer is able to detect sufficient spectral lines from many active binary and dMe stars to determine their coronal-emission-measure distributions. The Lyman/FUSE or next-generation spectrometers are needed to study solar-type stars or flaring stars with high time resolution. The high throughput and effective area of a nex-generation spectrometer is needed for Doppler imaging studies, stellar wind and downflow measurements, and high time and spectral resolution of stellar flares.
Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers from 0.40 to 0.93 of a 45 degree sweptback wing of aspect ratio 4
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Some Effects of Chordwise Fences on the Aerodynamic Characteristics of Four Moderately Sweptback Wings in the Low-lift Range at Transonic Mach Numbers and at Mach Number 1.9
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High-speed Aerodynamic Characteristics of a Lateral-control Model III : Section Characteristics, Fence Studies, and Tabulated Pressure Coefficients with Modified NACA 0012-64 Section, 26.6-percent-chord, Plain Aileron, 0 and 45 Degree Sweepback
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Wind tunnel investigation at low speed of a twisted and cambered wing swept back 63 degrees with vortex generators and fences
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Pressure Distribution at Mach Numbers up to 0.90 on a Cambered and Twisted Wing Having 40 Degrees of Sweepback and an Aspect Ratio of 10, Including the Effects of Fences
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Use of Fences to Increase Uniformity of Boundary Layer on Side Walls of Supersonic Wind Tunnels
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Effects of Chord Discontinuities and Chordwise Fences on Low-speed Static Longitudinal Stability of an Airplane Model Having a 35 Degree Sweptback Wing
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Effects of Twist and Camber, Fences, and Horizontal-tail Height on the Low-speed Longitudinal Stability Characteristics of a Wing-fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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The Effects of Leading-edge Extensions, a Trailing-edge Extension, and a Fence on the Static Longitudinal Stability of a Wing-fuselage-tail Combination Having a Wing with 35 Degrees of Sweepback and an Aspect Ratio of 4.5
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Wind-tunnel Investigation of the Effects of a Fence and a Leading-edge Notch on the Aerodynamic Loading Characteristics in Pitch of a 45 Degree Sweptback Wing at High Subsonic Speeds
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The Effects of Fences on the High-speed Longitudinal Stability of a Swept-wing Airplane
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