Wind-tunnel Investigation at Low Speeds to Determine Flow-field Characteristics and Ground Influence on a Model with Jet-augmented Flaps
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Vogler, Raymond D↗
Engineering topics
Turner, Thomas R
Publications and source records attributed to Turner, Thomas R.
Wind-tunnel Investigation of Jet-augmented Flaps on a Rectangular Wing to High Momentum Coefficients
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Lockwood, Vernard E↗
A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion
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Turner, Thomas R↗
Wind-tunnel investigation at transonic speeds of a jet control on a 35 degree swept wing : transonic-bump method
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Vogler, Raymond, D↗
Wind-tunnel investigation at transonic speeds of a jet control on an 80 degree delta-wing missile
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Turner, Thomas R↗
Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
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Turner, Thomas R↗
Low-speed wind-tunnel investigation of a jet control on a 35 degree swept wing
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Lowry, John, G↗
Effects of Rate of Flap Deflection on Flap Hinge Moment and Wing Lift Through the Mach Number Range from 0.32 to 0.87
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Turner, Thomas R↗
An investigation at transonic speeds of the effects of control chord and span on the control characteristics of a tapered wedge-type wing of aspect ratio 2.5 : transonic-bump method
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Vogler, Raymond D↗
Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
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Turner, Thomas R↗
Investigation at transonic speeds of a 35-percent-chord aileron on a tapered wedge-type wing of aspect ratio 2.5 with and without a fuselage
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Turner, Thomas R↗
Maximum-lift investigation of a 1/40-scale X-1 airplane wing at Mach numbers from 0.60 to 1.15
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Turner, Thomas R↗
Maximum-lift investigation at Mach numbers from 0.05 to 1.20 of a wing with leading edge swept back 42 degrees
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Turner, Thomas R↗
Aerodynamic Characteristics at Subsonic and Transonic Speeds of a 42.7 Degree Sweptback Wing Model Having an Aileron with Finite Trailing-edge Thickness
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Lockwood, Vernard E↗
Preliminary Investigation of Various Ailerons on a 42 Degree Sweptback Wing for Lateral Control at Transonic Speeds
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Turner, Thomas R↗
Pressure distribution over a plug-type spoiler-slot aileron on a tapered wing with full span slotted flaps
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AIRFOILS - NACA 230 - CHAR , MOMENTS & ORDINATES W↗
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail
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WING FLAPS, SPLIT - PARTIAL-SPAN (20%-CHORD)↗
Aerodynamic Characteristics and Flap Loads of Perforated Double Split Flaps on a Rectangular NACA 23012 Airfoil
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WING FLAPS, SPLIT (DOUBLE)(PERFORATED)↗