Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees
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Lowry, John G↗
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Low-speed longitudinal characteristics of a circular-arc 52 degree sweptback wing of aspect ratio 2.84 with and without leading-edge and trailing-edge flaps at Reynolds numbers from 1.6 x 10(exp 6) to 9.7 x 10(exp 6)
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Foster, Gerald V↗
Wind-tunnel Investigation of the Low-speed Longitudinal and Lateral Control Characteristics of a Triangular-wing Model of Aspect Ratio 2.31 Having Constant-chord Control Surfaces
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Wolhart, Walter D↗
The Low-speed Lift and Pitching Moment Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 with and Without High-lift and Stall-control Devices as Determined from Pressure Distribution at a Reynolds Number of 4.0 x 10(exp 6)
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Bollech, Thomas V↗
Low-speed Lateral Control Characteristics of an Unswept Wing with Hexagonal Airfoil Sections and Aspect Ratio 4.0 at a Reynolds Number of 6.2 x 10(exp 6)
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Hadaway, William M↗
Results of Initial Wind-tunnel Flutter Experiments at Low Speed with a Towed Airplane Model Having a 40 Degree Sweptback Wing of Aspect Ratio 3.62 Equipped with Pylon-mounted Stores
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Martina, Albert P↗
Low-speed wind-tunnel results for a thin aspect-ratio-1.85 pointed-wing-fuselage model with double slotted flaps
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Brown, Albert E↗
Wind-tunnel Investigation of the Low-speed Stability and Performance Characteristics of a Jet-powered Low-aspect-ratio Vertical-take-off-and-landing Configuration with Engines Buried in Tiltable Wings
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Scallion, William I↗
Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings
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AIRFOILS - NACA 0012↗
Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45 degrees sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons
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WIND TUNNEL TESTS - NACA-300 MPH (10 FEET X 7 FEET↗
Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6
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Jaquet, Byron M↗
Effect of Airfoil Profile of Symmetrical Sections on the Low-speed Static-stability and Yawing Derivatives of 45 Degrees Sweptback Wing Models of Aspect Ratio 2.61
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Letko, William↗
Investigation of the Effects of Wing and Tail Modifications on the Low-speed Stability Characteristics of a Model Having a Thin 40 Degree Swept Wing of Aspect Ratio 3.5
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Weil, Joseph↗
Low-speed Lateral-control Characteristics of an Unswept Wing with Hexagonal Airfoil Sections and Aspect Ratio 2.5 Equipped with Spoilers and with Sharp- and Thickened-trailing-edge Flap-type Ailerons at a Reynolds Number of 7.6 x 10(exp 6)
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Fitzpatrick, James E↗
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↗
Nacelle/pylon interference study on a 1/17th-scale, twin-engine, low-wing transport model
NASA-Langley has conducted wind tunnel tests of a twin-engine, low-wing transport aircraft configuration with 10.8-aspect ratio supercritical wing, in order to ascertain and compare the wing/nacelle interference effects of through-flow nacelled simulating 'superfan' very high bypass ratio (BPR=20) turbofans and current-technology (BPR=6) turbofans. Measurements of model forces and moments have been obtained, together with extensive external static pressure measurement on the model's wings, nacelles, and pylons in the Mach 0.5-0.8 range, at angles of attack in the -4 to +8 deg range. The superfan nacelles exhibit a significant advantage over current-technology turbofan nacelles, when the superfan's SFC gains are taken into account.
Pendergraft, Odis C., Jr.↗
Wind-tunnel Investigation at Low Speed of the Lateral Control Characteristics of an Unswept Untapered Semi-span Wing of Aspect Ratio 3.13 Equipped with Various 25-percent-chord Plain Ailerons
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AILERONS - POSITION↗
Low-speed Longitudinal Aerodynamic Characteristics of a Twisted and Cambered Wing of 45 Degree Sweepback and Aspect Ratio 8 with and Without High-lift and Stall-control Devices and a Fuselage at Reynolds Numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6
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Salmi, Reino J↗