An Aerodynamic Transition in Tiny Insect Flight
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Baseball Science Fun Sheets
WASHINGTON NATIONALS BASEBALL SCIENCE FUN SHEETS E SID AC T T U I V O I T Aerodynamics Y INTRODUCTION What is the difference between a curveball, fastball and cutter? In this lesson, students will KEY WORDS learn about the aerodynamic properties of a ball • Axis of Rotation in flight and the influence of spin on its trajectory. • Magnus Effect OBJECTIVES • Curveball • Determine the trajectory of different pitches. • Simulate different types of pitches using a ball. • Fastball • Explain why baseballs curve (Magnus Effect). KEY CONCEPTS • Aerodynamics is about the way something FOCUS STANDARDS moves when passing through air. In this Relates to Line of Symmetry: activity, students will measure the effect of changing the way a ball moves through air by CCSS.MATH.CONTENT.4.G.A.3 where it ends up. • Draw lines of symmetry of a ball. Relates to Coordinate Graphs: • Plot the distance a ball curves from the center CCSS.MATH.CONTENT.5.G.A.2 line. MATERIALS • Worksheet • Ball (beachball if available) • Tape Measure • Coins & Tape Aerodynamics PROCEDURE 1. Show a Magnus Effect video to engage the students. 2. Provide students with paper and tape. Roll the paper to create a hollow cylinder. 3. On a tilted platform, release the roll of paper. 4. The rotation of the paper and Magnus Effect will cause the cylinder to spin as it falls towards the floor. PROCEDURE 5. Draw a line1. S hofow symmetry the Magnus E fonfect thevideo ball to understand the rotational axis (vertical vs. horizontal). a. Provide students with paper and tape. Roll the paper to create a hollow cylinder. -
Describing Baseball Pitch Movement with Right-Hand Rules
Computers in Biology and Medicine 37 (2007) 1001–1008 www.intl.elsevierhealth.com/journals/cobm Describing baseball pitch movement with right-hand rules A. Terry Bahilla,∗, David G. Baldwinb aSystems and Industrial Engineering, University of Arizona, Tucson, AZ 85721-0020, USA bP.O. Box 190 Yachats, OR 97498, USA Received 21 July 2005; received in revised form 30 May 2006; accepted 5 June 2006 Abstract The right-hand rules show the direction of the spin-induced deflection of baseball pitches: thus, they explain the movement of the fastball, curveball, slider and screwball. The direction of deflection is described by a pair of right-hand rules commonly used in science and engineering. Our new model for the magnitude of the lateral spin-induced deflection of the ball considers the orientation of the axis of rotation of the ball relative to the direction in which the ball is moving. This paper also describes how models based on somatic metaphors might provide variability in a pitcher’s repertoire. ᭧ 2006 Elsevier Ltd. All rights reserved. Keywords: Curveball; Pitch deflection; Screwball; Slider; Modeling; Forces on a baseball; Science of baseball 1. Introduction The angular rule describes angular relationships of entities rel- ative to a given axis and the coordinate rule establishes a local If a major league baseball pitcher is asked to describe the coordinate system, often based on the axis derived from the flight of one of his pitches; he usually illustrates the trajectory angular rule. using his pitching hand, much like a kid or a jet pilot demon- Well-known examples of right-hand rules used in science strating the yaw, pitch and roll of an airplane. -
Investigation of the Factors That Affect Curved Path of a Smooth Ball
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by TED Ankara College IB Thesis Oğuz Kökeş D1129‐063 Physics Extended Essay Investigation Of The Factors That Affect Curved Path Of A Smooth Ball Oğuz Kökeş D1129‐063 School: TED Ankara Collage Foundation High School Supervisor: Mr. Özgül Kazancı Word Count: 3885 1 Oğuz Kökeş D1129‐063 Abstract This essay is focused on an investigation of spin(revolution per second) of a ball and its effect on the ball’s curved motion in the air. When a ball is hit and spinning in the air, it leaves its straight route and follows a curved path instead. In the following experiment the reasons and results of this curved path (deflection) is examined. In the experiment, the exerted force on the ball and its application point on the ball is changed. The ball was hit by 3 different tension levels of a spring mechanism and their deflection values were measured. Spin of the ball was also recorded via a video camera. Likewise, the location of the spring mechanism was also changed to hit from close to the end and the geometric center of the ball. The spin of the ball was also recorded and its deflection was measured. By analysing this experiment, one can see that the spin of a ball is an important factor in its curve. The curve of a ball can be increased by spinning it more in the air. So to create more spin one can increase the exerted force on the ball or apply the force close to the end of the ball. -
Computational Turbulent Incompressible Flow
This is page i Printer: Opaque this Computational Turbulent Incompressible Flow Applied Mathematics: Body & Soul Vol 4 Johan Hoffman and Claes Johnson 24th February 2006 ii This is page iii Printer: Opaque this Contents I Overview 4 1 Main Objective 5 2 Mysteries and Secrets 7 2.1 Mysteries . 7 2.2 Secrets . 8 3 Turbulent flow and History of Aviation 13 3.1 Leonardo da Vinci, Newton and d'Alembert . 13 3.2 Cayley and Lilienthal . 14 3.3 Kutta, Zhukovsky and the Wright Brothers . 14 4 The Navier{Stokes and Euler Equations 19 4.1 The Navier{Stokes Equations . 19 4.2 What is Viscosity? . 20 4.3 The Euler Equations . 22 4.4 Friction Boundary Condition . 22 4.5 Euler Equations as Einstein's Ideal Model . 22 4.6 Euler and NS as Dynamical Systems . 23 5 Triumph and Failure of Mathematics 25 5.1 Triumph: Celestial Mechanics . 25 iv Contents 5.2 Failure: Potential Flow . 26 6 Laminar and Turbulent Flow 27 6.1 Reynolds . 27 6.2 Applications and Reynolds Numbers . 29 7 Computational Turbulence 33 7.1 Are Turbulent Flows Computable? . 33 7.2 Typical Outputs: Drag and Lift . 35 7.3 Approximate Weak Solutions: G2 . 35 7.4 G2 Error Control and Stability . 36 7.5 What about Mathematics of NS and Euler? . 36 7.6 When is a Flow Turbulent? . 37 7.7 G2 vs Physics . 37 7.8 Computability and Predictability . 38 7.9 G2 in Dolfin in FEniCS . 39 8 A First Study of Stability 41 8.1 The linearized Euler Equations . -
A Review of the Magnus Effect in Aeronautics
Progress in Aerospace Sciences 55 (2012) 17–45 Contents lists available at SciVerse ScienceDirect Progress in Aerospace Sciences journal homepage: www.elsevier.com/locate/paerosci A review of the Magnus effect in aeronautics Jost Seifert n EADS Cassidian Air Systems, Technology and Innovation Management, MEI, Rechliner Str., 85077 Manching, Germany article info abstract Available online 14 September 2012 The Magnus effect is well-known for its influence on the flight path of a spinning ball. Besides ball Keywords: games, the method of producing a lift force by spinning a body of revolution in cross-flow was not used Magnus effect in any kind of commercial application until the year 1924, when Anton Flettner invented and built the Rotating cylinder first rotor ship Buckau. This sailboat extracted its propulsive force from the airflow around two large Flettner-rotor rotating cylinders. It attracted attention wherever it was presented to the public and inspired scientists Rotor airplane and engineers to use a rotating cylinder as a lifting device for aircraft. This article reviews the Boundary layer control application of Magnus effect devices and concepts in aeronautics that have been investigated by various researchers and concludes with discussions on future challenges in their application. & 2012 Elsevier Ltd. All rights reserved. Contents 1. Introduction .......................................................................................................18 1.1. History .....................................................................................................18 -
Flexural Stiffness Patterns of Butterfly Wings (Papilionoidea)
35:61–77,Journal of Research1996 (2000) on the Lepidoptera 35:61–77, 1996 (2000) 61 Flexural stiffness patterns of butterfly wings (Papilionoidea) Scott J. Steppan Committee on Evolutionary Biology, University of Chicago, Chicago, IL 60637, USA., E-mail: [email protected] Abstract. A flying insect generates aerodynamic forces through the ac- tive manipulation of the wing and the “passive” properties of deformability and wing shape. To investigate these “passive” properties, the flexural stiffness of dried forewings belonging to 10 butterfly species was compared to the butterflies’ gross morphological parameters to determine allom- etric relationships. The results show that flexural stiffness scales with wing 3.9 loading to nearly the fourth power (pw ) and is highly correlated with wing area cubed (S3.1). The generalized map of flexural stiffness along the wing span for Vanessa cardui has a reduction in stiffness near the distal tip and a large reduction near the base. The distal regions of the wings are stiffer against forces applied to the ventral side, while the basal region is much stiffer against forces applied dorsally. The null hypothesis of structural isom- etry as the explanation for flexural stiffness scaling is rejected. Instead, selection for a consistent dynamic wing geometry (angular deflection) in flight may be a major factor controlling general wing stiffness and deformability. Possible relationships to aerodynamic and flight habit fac- tors are discussed. This study proposes a new approach to addressing the mechanics of insect flight and these preliminary results need to be tested using fresh wings and more thorough sampling. KEY WORDS: biomechanics, butterfly wings, flight, allometry, flexural stiff- ness, aerodynamics INTRODUCTION A flying insect generates aerodynamic forces primarily through the ac- tive manipulation of wing movements and the “passive” morphological prop- erties of deformability and wing shape. -
The Flight of the Bumble
The Flight of the Bumble Bee Grade Span 4 Subject Area • Science • Math Materials • Fab@School Maker Studio • Digital fabricator or scissors • 65lb or 110lb cardstock • Pencils, pens, markers, or crayons • Stapler, tape, or glue Online Resources • Website: The Physics- There is a common myth that bumble bees defy the laws of Defying Flight of the physics as they apply to aerodynamics. Basically, they shouldn’t Bumblebee be able to fly. Using high-speed photography, Michael Dickinson, • Website: Bumblebees Can a professor of biology and insect flight expert at the University of Fly Into Thin Air Washington, published an article in 2005 all about the why and how the bumblebee takes flight. Through this Fab@School Maker Studio • Video: Bumble Bee in Slow activity, your students will examine the anatomy of a bumblebee or Motion other flying insect. • Article: Lasers Illuminate the Flight of the Bumblebee • PDF: Fab@School Quick Objective Start Guide Author • Using Fab@School Maker Studio, students will design a 2D Denine Jimmerson, or 3D prototype of a bumble bee (or another flying insect) Executive Director of that demonstrates how its structure serves it in its function Curriculum and Design, of flight. FableVision Learning © 2017 FableVisionLearning, LLC • The Flight of the Bumble Bee www.FableVisionLearning.com • [email protected] 1 Fab@School Maker Studio • www.FabMakerStudio.com Big Idea Challenge Functions help to determine form. Show the Bumble Bee in Slow Motion video to your students. Pose the question: How do bees fly? Driving Question How do bees fly? Explain to the students that they will be researching how bumble bees (or other insects/animals) fly. -
The Novel Aerodynamics of Insect Flight: Applications to Micro-Air Vehicles
The Journal of Experimental Biology 202, 3439–3448 (1999) 3439 Printed in Great Britain © The Company of Biologists Limited 1999 JEB2214 THE NOVEL AERODYNAMICS OF INSECT FLIGHT: APPLICATIONS TO MICRO-AIR VEHICLES C. P. ELLINGTON* Department of Zoology, University of Cambridge, Downing Street, Cambridge CB2 3EJ, UK *e-mail: [email protected] Accepted 15 September; published on WWW 16 November 1999 Summary The wing motion in free flight has been described for accompanies repeated clapping of the wings, but the spiral insects ranging from 1 to 100 mm in wingspan. To support LEV can be used to augment the lift production of the body weight, the wings typically produce 2–3 times propellers, rotors and micro-air vehicles (MAVs). Design more lift than can be accounted for by conventional characteristics of insect-based flying machines are aerodynamics. Some insects use the fling mechanism: the presented, along with estimates of the mass supported, the wings are clapped together and then flung open before the mechanical power requirement and maximum flight speeds start of the downstroke, creating a lift-enhancing vortex over a wide range of sizes and frequencies. To support a around each wing. Most insects, however, rely on a leading- given mass, larger machines need less power, but smaller edge vortex (LEV) created by dynamic stall during ones operating at higher frequencies will reach faster flapping; a strong spanwise flow is also generated by the speeds. pressure gradients on the flapping wing, causing the LEV to spiral out to the wingtip. Technical applications of the Key words: insect, flight, aerodynamics, flapping flight, micro-air fling are limited by the mechanical damage that vehicle. -
Numerical Investigation of the Magnus Effect on Dimpled Spheres
NUMERICAL INVESTIGATION OF THE MAGNUS EFFECT ON DIMPLED SPHERES Nikolaos Beratlis Elias Balaras Mechanical and Aerospace Engineering Department of Mechanical Arizona State University and Aerospace Enginering Tempe, AZ, USA George Washington University [email protected] Washington, DC, USA [email protected] Kyle Squires Mechanical and Aerospace Enginering Arizona State University Tempe, AZ, USA [email protected] ABSTRACT 0.5 An efficient finite-difference, immersed-boundary, k 0.4 3 k2 Navier-Stokes solver is used to carry out a series of sim- k1 ulations of spinning dimpled spheres at three distinct flow 0.3 D regimes: subcritical, critical and supercritical. Results exhibit C 0.2 all the qualitative flow features that are unique in each regime, golf ball smooth namely the drag crisis and the alternation of the Magnus 0.1 effect. 0 5 6 10 Re 10 Figure 1. Variation of CD vs Re for a smooth sphere Achen- INTRODUCTION bach (1972), –; spheres with sand-grained roughness Achen- Golf ball aerodynamics are of particular importance not −5 −5 bach (1972), −− (k1 = k=d = 1250×10 , k2 = 500×10 , only due to the quest for improved performance of golf balls − k = 150 × 10 5); golf ball Bearman & Harvey (1976), ·−. but also because of the fundamental phenomena associated 3 with the drag reduction due to dimples. Dimples are known to lower the critical Reynolds number at which a sudden drop in the drag is observed. Figure 1, for example, shows the tion caused by dimples. Using hot-wire anemometry they drag coefficient, CD, as a function of the Reynolds number, measured the streamwise velocity within individual dimples Re = UD=n, (where D is the diameter of the golf ball, U the and showed that the boundary layer separates locally within velocity and n the kinematic viscosity of the air) for a golf ball the dimples. -
Karlstad University Faculty for Health, Science and Technology Mathematics of Football Free Kicks Analytic Mechanics FYGB08
Karlstad University Faculty for Health, Science and Technology Robin Lundström February 4, 2019 Mathematics of football free kicks Analytic Mechanics FYGB08 Abstract A direct free kick is a method of restarting play in a game of football that is awarded to a team following a foul from the opposing team. Free kicks are situations that professional footballers have been practicing daily, with world class coaches, for the majority of their life, however the conversion rate of a free kick is somewhere between 0 − 10% depending on where the free kick is taken. In this report the physics of free kicks was investigated by analyzing a ball of which gravitational force, drag force and the Magnus force were acting on the ball. The purposes of the report were to both describe the trajectory of a football and to investigate the low conversion rate of direct free kicks. The mathematics of free kicks was implemented in MatLab and simulations are consistent with the physical intuition experienced when watching a game. It was concluded that small deviations of the initial conditions made a great impact on the trajectory. 1 Contents 1 Introduction 2 2 Theory 2 2.1 Declaration of variables and notation.....................................2 2.2 Gravitational force...............................................3 2.3 Drag force....................................................4 2.4 The Magnus effect...............................................4 3 Method 5 4 Results 5 4.1 Implementing forces in Matlab........................................5 4.2 Implementing a football freekick in Matlab.................................7 4.2.1 The wall.................................................7 4.2.2 The goalkeeper.............................................7 4.3 Simulation results...............................................7 4.3.1 Different models............................................8 4.4 Monte Carlo simulations............................................8 5 Discussion 11 5.1 Conclusion.................................................. -
Study of Turning Takeoff Maneuver in Free-Flying Dragonflies
Study of turning takeoff maneuver in free-flying dragonflies: effect of dynamic coupling Samane Zeyghami1, Haibo Dong2 Mechanical and Aerospace Engineering, University of Virginia, VA, 22902 SUMMARY Turning takeoff flight of several dragonflies was recorded, using a high speed photogrammetry system. In this flight, dragonfly takes off while changing the flight direction at the same time. Center of mass was elevated about 1-2 body lengths. Five of these maneuvers were selected for 3D body surface reconstruction and the body orientation measurement. In all of these flights, 3D trajectories and transient rotations of the dragonfly’s body were observed. In oppose to conventional banked turn model, which ignores interactions between the rotational motions, in this study we investigated the strength of the dynamic coupling by dividing pitch, roll and yaw angular accelerations into two contributions; one from aerodynamic torque and one from dynamic coupling effect. The latter term is referred to as Dynamic Coupling Acceleration (DCA). The DCA term can be measured directly from instantaneous rotational velocities of the insect. We found a strong correlation between pitch and yaw velocities at the end of each wingbeat and the time integral of the corresponding DCA term. Generation of pitch, roll and yaw torques requires different aerodynamic mechanisms and is limited due to the other requirements of the flight. Our results suggest that employing DCA term gives the insect capability to perform a variety of maneuvers without fine adjustments in the aerodynamic torque. Key words: insect flight, aerial maneuver, dragonfly, pitch. INTRODUCTION Aerial maneuvers of different insect species are studied widely in the last decades and many aspects of maneuverability in insect flight are explored. -
Dragonfly Flight Quick Z
Dragonfly flight quick Z. Jane Wang Dragonflies have evolved for about 350 million years. What kinds of study aerodynamic tricks have they discovered? Jane Wang is an associate professor of theoretical and applied mechanics at Cornell University in Ithaca, New York. Summer in Ithaca, New York, is a good time to watch tional to the product of velocity squared, fluid density, and dragonflies. At a glance, you can see that a dragonfly has a wing area. That product can be interpreted as the rate of prominent head, an elongated body, and two pairs of slender momentum transfer from air particles that hit the wing and wings extending to each side. As it takes off, the wings appear bounce off. But if the particle picture were the whole story, as a blur. In air, the dragonfly dances in unpredictable steps, planes would not be able to carry much nor would they be hovering briefly then quickly moving to a new location. Just very efficient. Based on the particle picture, one would pre- when you think it might stay long enough in the viewfinder dict—as Isaac Newton did—a lift proportional to sin2α for a of your camera, poof! It is gone. In contrast, an airplane, noisy wing with angle of attack α. That’s much smaller than ob- and powerful, has a more straightforward way of going about served, at least for a small angle of attack. The same calcula- its business. Propelled by engines and lifted by wings, it wastes tion also predicts a maximum lift-to-drag ratio of 1 at an no time in going from one place to another.