Andere Kunden interessierten sich auch für
![Experimental Methods to Characterize Nonlinear Vibration of Flapping Wing Micro Air Vehicles]( "Experimental Methods to Characterize Nonlinear Vibration of Flapping Wing Micro Air Vehicles")
Experimental Methods to Characterize Nonlinear Vibration of Flapping Wing Micro Air Vehicles59,99 €![Flapping Wing Micro Air Vehicle Wing Manufacture and Force Testing]( "Flapping Wing Micro Air Vehicle Wing Manufacture and Force Testing")
Flapping Wing Micro Air Vehicle Wing Manufacture and Force Testing59,99 €![Biomimetic Micro Air Vehicle Testing Development and Small Scale Flapping-Wing Analysis]( "Biomimetic Micro Air Vehicle Testing Development and Small Scale Flapping-Wing Analysis")
Biomimetic Micro Air Vehicle Testing Development and Small Scale Flapping-Wing Analysis59,99 €![Laser Dot Projection Photogrammetry and Force Measurement for Flapping Wing Micro Air Vehicles]( "Laser Dot Projection Photogrammetry and Force Measurement for Flapping Wing Micro Air Vehicles")
Laser Dot Projection Photogrammetry and Force Measurement for Flapping Wing Micro Air Vehicles59,99 €![Least-Squares Finite Element Formulation for Fluid-Structure Interaction]( "Least-Squares Finite Element Formulation for Fluid-Structure Interaction")
Least-Squares Finite Element Formulation for Fluid-Structure Interaction59,99 €![The Development of a Finite Element Program to Model High Cycle Fatigue in Isotropic Plates]( "The Development of a Finite Element Program to Model High Cycle Fatigue in Isotropic Plates")
The Development of a Finite Element Program to Model High Cycle Fatigue in Isotropic Plates59,99 €![Modeling, Stability, and Control of a Rotatable Tail on a Micro Air Vehicle]( "Modeling, Stability, and Control of a Rotatable Tail on a Micro Air Vehicle")
Modeling, Stability, and Control of a Rotatable Tail on a Micro Air Vehicle59,99 €
The development and use of Micro Air Vehicles is becoming more and more important to the military. Size, weight, maneuverability, stealth, and fuel consumption are just some of the constraints on a future Micro Air Vehicle. Perfect blueprints for a small scale flying machine are both insects and humming birds. Medium sized hummingbirds are found to have wings-beats at a frequency of 18-28 Hz. There is a vast amount of complexity to just how these creatures can create lift; however, this study looks at different beams made of common materials with 1st natural bending frequencies in this range. This study documents and evaluates the use of analytical tools to solve for nonlinear characteristics of a system. A function called the backbone curve is incorporated into a MATLAB program. The Hilbert transform characterized by the nonlinear decrement approach captures all of the necessary coefficients for this function. ABAQUS/CAE is relied upon. The numerical finite element results are compared to experiments. This work gives a better understanding of how materials and geometry perform when used in Micro Air Vehicle design considering large displacements.