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Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
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A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2
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Blade-mounted flap control for BVI noise reduction proof-of-concept test
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Interference on a model afterbody from downstream support hardware at transonic Mach numbers
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Simulated rotor test apparatus dynamic characteristics in the 80- by 120-foot wind tunnel
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Experimental studies of shock-wave/wall-jet interaction in hypersonic flow
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Effect of in-flight ice accretion on the performance of a multi-element airfoil
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Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
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Pressure probe designs for dynamic pressure measurements in a supersonic flow field
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Some buffet response characteristics of a twin-vertical-tail configuration
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Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack
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Shock-tunnel combustor testing for hypersonic vehicles
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Design and fabrication of the NASA decoupler pylon for the F-16 aircraft
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Semi-span model testing in the National Transonic Facility
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Boundary layer transition studies
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Investigation of solid plume simulation criteria to produce flight plume effects on mulitbody configuration in wind tunnel tests
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Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models
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Supersonic laminar flow control research
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Measurements of unsteady pressure and structural response for an elastic supercritical wing
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Image processing of aerodynamic data
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Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
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Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
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Analysis of wind tunnel oscillatory data of the X-31A aircraft
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Contraction design for small low-speed wind tunnels
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