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industrie mécanique - iate.europa.eu
industrie mécanique - iate.europa.eu
Low-speed wind-tunnel investigation of a thiangularswept!backalrinlrtlnthnA low-speed investigation has been conducted in the Langley two-dtiensional low-turbulence tunnel to study a sweptback wing-root air-inlet configuration believed suitable for transonic-speed jet-powered airplanes....
général - core.ac.uk - PDF: digital.library.unt.edu
Aerodynamic characteristics of a delta wing at high angles of attackb = half span length c = wing root chord length CN = normal force coefficient CMP = pitching moment coefficient about the apex of the wing CMR = rolling moment coefficient about the wing root Cp = local...
Wind-tunnel investigation of a large-scale vtol aircraft model with wing root and wing thrust augmentors...1.65 with augmentors located in the wing root and the wing trailing edge....
Effect of wing sweep, angle of attack, reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration [electronic resource] /... One wing root of each model was faired to the fuselage with a fillet....
Design of wing root rotation mechanism for dragonfly-inspired micro air vehicleThis paper proposes a wing root control mechanism inspired by the drag-based system of a dragonfly....


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