Experimental Investigation of the Drag Due to Wedges Along the Trailing Edge of a Swept Wing
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Gambucci, Bruno J↗
Engineering topics
Gambucci, Bruno J
Publications and source records attributed to Gambucci, Bruno J.
Effects of Modifications to a Control Surface on a 6-percent-thick Unswept Wing on the Transonic Control-surface Flutter Derivatives
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Wyss, John A↗
Perforated Sheets as the Porous Material for a Suction-flap Application
Two-dimensional tests were made of an NACA 0006 airfoil with area suction applied to a porous region on a 0.3-chord trailing-edge flap deflected 50 degrees. The lift with suction approached the value computed from thin-airfoil theory. The lift gains and suction quantity requirements were unaffected by the perforation patterns of the surface over a wide range of hole sizes and spacings.
MATERIALS - TYPES↗
Section Characteristics of the NACA 0006 Airfoil with Leading-edge and Trailing-edge Flaps
Lift and pitching-moment characteristics of an NACA 0006 airfoil are presented for various deflections of a 0.15-chord leading-edge flap and a 0.30-chord plain trailing-edge flap. Pressure-distribution data are presented in tabular form. The data were obtained at a Mach number of 0.15 and a Reynolds number of 4,500,000.
FLAPS, PLAIN - WING SECTIONS↗
Perforated Sheets as a Porous Material for Distributed Suction and Injection
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Dannenberg, Robert E↗
A Fibrous-glass Compact as a Permeable Material for Boundary-layer Control Applications Using Area Suction
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Dannenberg, James A↗
The Resistance to Air Flow of Porous Materials Suitable for Boundary-layer-control Applications Using Area Suction
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Dannenberg, Robert E↗
Boundary-layer measurements on several porous materials with suction applied
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Mccullough, George B↗