Flow control is a field of fluid dynamics. It involves a small configuration change to serve an ideally large engineering benefit, like drag reduction, lift increase, mixing enhancement or noise reduction. This change may be accomplished by passive or active devices.
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Passive vs active
Passive devices by definition require no energy. Passive techniques include turbulators or roughness elements geometric shaping, the use of vortex generators, and the placement of longitudinal grooves or riblets on airfoil surfaces.
Active control requires actuators that require energy and may operate in a time-dependent manner.[1] Active flow control includes steady or unsteady suction or blowing,[2] the use of synthetic jets, valves and plasma actuators. Actuation may be pre-determined (open-loop control) or be dependent on monitoring sensors (closed-loop control).
Aircraft wings
Airplane wing performance has a substantial effect on not only runway length, approach speed, climb rate, cargo capacity, and operation range but also noise and emissions. Wing performance can be degraded by flow separation, which depends on the aerodynamic characteristics of the airfoil. Aerodynamic and non-aerodynamic constraints often conflict. Flow control is required to overcome such difficulties. Techniques developed to manipulate the boundary layer, either to increase lift or decrease drag, and separation delay come under the general heading of flow control.
Aurora Flight Sciences is a DARPA CRANE (Control of Revolutionary Aircraft with Novel Effectors) grantee. It initially involved testing a small-scale plane that uses compressed air bursts instead of external moving parts such as flaps. The program seeks to eliminate the weight, drag, and mechanical complexity involved in moving control surfaces. The air bursts modify the air pressure and flow, and change the boundaries between streams of air moving at different speeds. The company built a 25% scale prototype with 11 conventional control surfaces, as well as 14 banks fed by eight air channels.[3] In 2023, the aircraft received its official designation as X-65.[4] In January 2024, DARPA and Aurora started CRANE Phase 3, building the first full-scale X-65 aircraft using active flow control actuators for primary flight control.[5][6] The 7,000-pound X-65 will be rolled out in early 2025 with the first flight planned for summer of 2025.[7]
References
- ^ Yousefi, Kianoosh; Saleh, Reza (2015-01-23). "Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing" (PDF). Meccanica. 50 (6): 1481–1494. doi:10.1007/s11012-015-0100-9. ISSN 0025-6455. S2CID 254797703.
- ^ Yousefi, Kianoosh; Saleh, Reza; Zahedi, Peyman (2014-05-01). "Numerical study of blowing and suction slot geometry optimization on NACA 0012 airfoil" (PDF). Journal of Mechanical Science and Technology. 28 (4): 1297–1310. doi:10.1007/s12206-014-0119-1. ISSN 1738-494X. S2CID 255532994.
- ^ Blain, Loz (2023-01-20). "Active flow control X-Plane uses virtual control surfaces made from air". New Atlas. Retrieved 2023-01-23.
- ^ "DARPA Receives X-65 Designation For Active Flow Experiment | Aviation Week Network". aviationweek.com. Retrieved 2024-01-13.
- ^ Choudhury, Rizwan (2024-01-05). "DARPA greenlits construction of its X-65 technology demonstrator aircraft". interestingengineering.com. Retrieved 2024-01-13.
- ^ Tingley, Brett (January 4, 2024). "DARPA's wild X-65 CRANE aircraft aims for 1st flight in summer 2025". space.com. Retrieved January 13, 2024.
- ^ Hadley, Greg (2023-05-16). "Meet the X-65: DARPA's New Plane Has No External Control Surfaces". Air & Space Forces Magazine. Retrieved 2024-01-13.
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This page was last edited on 22 March 2024, at 04:25