Solar wind pressure variations and auroras
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solar wind auroras↗
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Results for “WIND PRESSURE”
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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Slow solar wind pressure pulses and their geoeffectiveness on the dayside aurora
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solar wind pulses geoeffectiveness aurora↗
The effect of static pressure-wind covariance on vertical carbon dioxide exchange at a windy subalpine forest site
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Burns, Sean P. (ORCID:0000000262581838)↗
Geomagnetic field variations caused by changes in the quiet-time solar wind pressure.
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Verzariu, P.↗
Results of a low speed approach and landing experimental investigation of a 0.050-scale space shuttle orbiter model (39-0) in the NASA/Ames Research Center's 12-foot pressure wind tunnel (0A101), volume 6
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Mulfinger, R. H.↗
Results of a low speed approach and landing experimental investigation of a 0.050-scale space shuttle orbiter model (39-0) in the NASA/Ames Research Center's 12-foot pressure wind tunnel (OA101), volume 5
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Mulfinger, R. H.↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel I : Characteristics of a Plain Wing
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Johnson, Ben H , Jr↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel III : the Effectiveness and Hinge Moments of a Skewed Wing-tip Flap
Results of wind-tunnel tests of a semispan model of a triangular wing of aspect ratio 2 with a skewed wing-tip flap are presented. Lift, drag, pitching-moment, and hinge-moment data are included for subsonic Mach numbers up to 0.95. The flap showed extremely high hinge moments and low effectiveness as a longitudinal control. Although less affected by compressibility, this flap is indicated to be inferior to a constant-chord flap when applied to this triangular wing.
MACH NUMBER EFFECTS - COMPLETE WINGS↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel II : The Effect of Constant-chord Leading- and Trailing-edge Flaps on the Low-speed Characteristics of the Wing
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Bandettini, Angelo↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel II : the Effectiveness and Hinge Moments of a Constant-chord Plain Flap
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Stephenson, Jack D↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel III : the Effectiveness of a Constant-chord Aileron
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Johnson, Ben H , Jr↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel IV : the Effect of a Constant-chord Leading-edge Flap at High Subsonic Speeds
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Reed, Verlin D↗
Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel I : the Effect of Reynolds Number and Mach Number on the Aerodynamic Characteristics of the Wing with Flap Undeflected
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Edwards, George G↗
Tests of a Model Horizontal Tail of Aspect Ratio 4.5 in the Ames 12-foot Pressure Wind Tunnel I : Quarter-chord Line Swept Back 35 Degrees
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Tinling, Bruce E↗
Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel V : Static Longitudinal Stability and Control Throughout the Subsonic Speed Range of a Semispan Model of a Supersonic Airplane
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Johnson, Ben H , Jr↗
Investigation in the Ames 12-foot Pressure Wind Tunnel of a Model Horizontal Tail of Aspect Ratio 3 and Taper Ratio 0.5 Having the Quarter-chord Line Swept Back 45 Degrees
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Kolbe, Carl D↗
Wind Pressure Distributions at Low Lift for the XF-92A Delta-wing Airplane at Transonic Speeds
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Keener, Earl R↗
Multipoint Cluster Observations of Kinetic Alfvén Waves, Electron Energization, and O + Ion Outflow Response in the Mid‐Altitude Cusp Associated With Solar Wind Pressure and/or IMF B Z Variations
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Arthur J. Hull↗