Simulation of reconfigurable Heli-UAV's using main rotor RPM control in failure modes



ARIEL, PD; AGGARWALA, BD; Tezer, Münevver (Wiley, 1988-01-01)
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Eyi Yumuşak, Mine; Eralp, Osman Cahit; Department of Mechanical Engineering (1993)
Simulation of Reinforced Concrete Member Response Using Lattice Model
Aydın, Beyazıt Bestami; Tuncay, Kağan; Binici, Barış (2019-09-01)
Lattice models are well suited for crack simulations; however, their use has been mostly limited to the fracture of plain concrete. In this study, a practical two-dimensional mesoscale lattice composed of overlapping elements was employed to simulate the monotonic response of reinforced concrete elements. The force-deformation response of each element is calibrated from direct tension tests. An explicit time integration technique with novel proportional-integral-derivative control is used to efficiently sim...
Simulation of Helicopter Shipboard Launch and Recovery with Time Accurate Airwakes
Lee, Dooyong; Joseph F, Horn; Sezer Uzol, Nilay; Long, Lyle N (2003-05-08)
Simulation of helicopter shipboard launch and recovery with time-accurate airwakes
Lee, Dooyong; Sezer Uzol, Nilay; Horn, Joseph F.; Long, Lyle N. (2005-01-01)
A simulation of the helicopter/ship dynamic interface has been developed and applied to simulate a UH-60A operating from a landing helicopter assault (LHA) class ship. Steady and time-accurate inviscid computational-fluid-dynamics (CFD) simulations are performed over a full-scale LHA class ship using the parallel flow solver PUMA2 to predict the unsteady vortical ship airwake. Time-accurate CFD solutions of the LHA airwake are interfaced with a flight dynamics simulation based on the GENHEL model. The fligh...
Citation Formats
İ. Yavrucuk, “Simulation of reconfigurable Heli-UAV’s using main rotor RPM control in failure modes,” 1999, Accessed: 00, 2020. [Online]. Available: