Effect of Area-suction-type Boundary-layer Control on the Landing-approach Characteristics of a 35 Degree Swept-wing Fighter
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Cooper, George E↗
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Flight Measurements of the Low-speed Characteristics of a 35 Degree Swept-wing Airplane with Area Suction Boundary-layer Control on the Flaps
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Anderson, Seth B↗
Investigation of the Use of Area Suction to Increase the Effectiveness of Trailing-edge Flaps of Various Spans on a Wing of 45 Degree Sweepback and Aspect Ratio 6
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Griffin, Roy N , Jr↗
Performance Characteristics of an Underslung Vertical-wedge Inlet with Porous Suction at Mach Numbers of 0.63 and 1.5 to 2.0
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Allen, John L↗
Stability of Supersonic Inlets at Mach 1.91 with Air Injection and Suction
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Kowalski, K↗
Application of Area Suction to Leading-edge and Trailing-edge Flaps on a 44 Degree Swept-wing Model
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Holzhauser, Curt A↗
The Use of Area Suction for Improving the Longitudinal Characteristics of a Thin Unswept Wing-fuselage Model with Leading- and Trailing-edge Flaps
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Koenig, David G↗
Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 with Area Suction Applied to Trailing-edge Flaps and with Several Wing Leading-edge Modifications
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Koenig, David G↗
Wind-tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-wing Airplane with Slotted Flaps, Area-suction Flaps, and Wing Leading-edge Devices
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Maki, Ralph L↗
Experimental Investigation of a High Subsonic Mach Number Turbine Having Low Rotor Suction-surface Diffusion
The quasi-three-dimensional method for the aerodynamic design of both stator and rotor blades is presented for a turbine having high weight flow and high specific work output. The turbine was designed for a relative critical velocity ratio of 0.82 at the rotor hub inlet. At the condition of equivalent design work output and blade speed, the efficiency based on the overall actual total-pressure ratio was 0.875, which is almost at high as those obtained for conservatively designed turbines.
Hauser, Cavour H↗
A Flight Investigation of Area-suction and Blowing Boundary-layer Control on the Trailing-edge Flaps of a 35 Degree Swept-wing-carrier-type Airplane
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Quigley, Hervey C↗
Flight Investigation of the Low-speed Characteristics of a 35 Degree Swept-wing Airplane Equipped with an Area-suction Ejector Flap and Various Wing Leading-edge Devices
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Anderson, Seth B↗
The Use of a Leading-edge Area-suction Flap and Leading-edge Modifications to Improve the High-lift Characteristics of an Airplane Model with a Wing of 45 Degree Sweep and Aspect Ratio 2.8
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Koenig, David G↗
Experimental Investigation of a High Subsonic Mach Number Turbine Having a 40-blade Rotor with Zero Suction-surface Diffusion
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Nusbaum, William J↗
Wind-tunnel Investigation of the Use of Leading-edge and Trailing-edge Area-suction Flaps on a 13-percent-thick Straight Wing and Fuselage Model
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Holzhauser, Curt A↗
Experimental Investigation of a High Subsonic Mach Number Turbine Having High Rotor Blade Suction-surface Diffusion
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Nusbaum, William J↗
Investigation of transonic turbine designed for zero diffusion of suction-surface velocity
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Whitney, Warren↗
Experimental Investigation of Boundary-layer Suction Through Slots to Obtain Extensive Laminar Boundary Layers on a 15-percent-thick Airfoil Section at High Reynolds Numbers
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Loftin, Laurence K , Jr↗