In aircraft design, a chine is a longitudinal line of sharp change in the cross-section profile of the fuselage or similar body. The term chine originates in boatbuilding, where it applies to a sharp profile change in the hull of a boat. In a flying boat hull or floatplane float, the longitudinal line of sharp change in cross … See more A chine can in aerodynamic terms act as a long extension of the wing root along the fuselage. Such chines first appeared on the Lockheed A-12 precursor of the SR-71 Blackbird, where they ran forward from the wing roots along … See more Large chines along the forward fuselage can have a significant effect on aircraft lift, drag, longitudinal balance and directional stability. Effect at high Mach … See more • Blended wing body See more WebJan 1, 2013 · Study on flow behavior and structure over chined fuselage at high angle of attack. Science China Technological Sciences, 53 (8) (2010), pp. 2057-2067. CrossRef View in Scopus Google Scholar [6] Erickson, G.E., Brandon, J.M., 1987. “On the nonlinear aerodynamic and stability characteristics of a generic chine-forebody slender- wing …

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WebMay 20, 2024 · Interestingly, while Northrop Grumman's LongShot concept has stealthy features, including a chined fuselage, it is shown carrying a pair of missiles externally, which would increase its overall ... Webthe thing always in this always was cruise performance. A canard surface would move the center of lift forward, which might be good for cruise performance, since a less stable aircraft (an aircraft with its center of gravity closer to the center of lift) reacts better to control surface movement, meaning you need to deflect the surface less to get a reaction. during cruise … chimney tablecloth

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WebSep 3, 2015 · 2.1 Experimental model. The experimental model is a wing-body configuration, which consists of a chined fuselage and a moderate swept wing, as illustrated in Fig. 1.The chined fuselage has a length of L = 680 mm, base width of D = 80 mm, and base height of H = 70 mm.All transversal cross sections of the fuselage are … WebMany traditional data bases, which involved smooth-sided forebodies, are no longer relevant for designing advanced aircraft. The current work provides data on the impact of chined … WebAug 1, 2015 · According to the evolution of flow with angle of attack, the leeward vortical flow over the chined fuselage can be divided into three regimes, which are regime of … grady goff chiropractor