...about the distribution of beak depth measurements in these two groups of medium ground finches? The shapes of the two graphs indicate that there is variability in the beak depth trait among the birds and that most birds have beak depth measurements that arrive right around the mean. 2. Compare the distribution of beak depths between survivors and nonsurvivors. In your answer, include the shape of the distributions, the range of the data, and the...
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...Miniature Aerial Vehicle – Airframe characterization R. Shivkumar, Hemendra Arya & K. Sudhakar Department of Aerospace Engineering Indian Institute of Technology Bombay Powai, Mumbai – 400076 e-mail: arya@aero.iitb.ac.in Abstract: Airframe design is an important step in the development of mini aerial vehicles. Airframe design means the shape and size of the aircraft. Issues related to mini aerial vehicle design are discussed in the paper. In this paper a case study of design of a 0.6 m fixed wing aerial vehicle is presented. This case study also brings out the requirement of various tools to conduct such an exercise. Introduction: Significant interest is being shown by academic institutions in research activities related to Remotely Piloted Vehicles (RPV’s) and Unmanned Aerial Vehicles (UAV’s). Flying platforms and their design with suitable payloads reinforce classroom education while exposing students to a host of flight related problems and issues of systems integration. There has been a long felt need to bring students, especially in the field of engineering, closer to the complexities and risks in dealing with actual systems. The Department of Aerospace Engineering, IIT Bombay has decided to make headway in this direction by developing remotely piloted aerial vehicles as experimental platforms[1]. The various disciplines required for such a design activity are aerodynamics, performance, structures, stability, control and propulsion. Each of these designs are different compared...
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...hours PIC Flight Test:________ % Private Pilot Licence Age: _______ Medical Category: __________ Written Test _______% (Must have valid Medical, ground school time and 10 hours flight time) Training: 45 hours total time 15 hours dual (3 hours dual cross country, 5 hours instrument training). 12 hours PIC (5 hours PIC cross country, including a 150 nm route with 2 stops) Flight Test: ______ % Night Rating Must hold a Private Pilot Licence Training: ______ hours of flight training consisting of: 5 more hours of instrument training 10 hours night (5 dual 2 hours cross country, 5 Solo, 10 takeoffs and landings) No Flight Test or Written Test VFR Over-The- Top (VFR OTT) Must hold a Private Pilot Licence Training: Minimum of 15 hours dual instrument time Multi-Engine Rating Training: No minimum hours required Flight Test Required Instrument Rating Group 1: _______; Group 2 ___________ Written and flight test required Training: 40 hours instrument time required (1 dual cross country 100 nm) Minimum 50 hour cross-country PIC AIRFRAMES AND PARTS OF AN AIRPLANE Basic Definitions Airframe: Structure of an aircraft without engines, power plants or instruments Fuselage: the body of the aircraft to which other components are attached, used to accommodate crew, passengers and cargo Wing: Device employed to develop lift on an airplane Ailerons: Surfaces hinged...
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...the nature of that organization. The subject is becoming more and more popular as people with diverse backgrounds and cultural values have to work together effectively and efficiently. Organizational behavior seeks to emphasize the understanding of behavior competencies in order to have an insight into how people are likely to behave as this knowledge is essential in controlling these behaviors and ensuring they are befitting to the achievement of organizational objectives. Whenever people interact in an organization many factors come into play and in this write up¸ we would be looking at a lot of factors associated with organizational behavior like culture, motivation, attitude and personalities, leadership and so on. We would be using wings café as our case study in understanding this concept while trying to bring fresh suggestions and ideas on how we think it should be managed and operated. Literature review The introduction of the concept of organizational culture has generally been attributed to several individuals, including Hofstede (1980) and Schein (1985). Although organizational culture has been defined in various ways, the definitions share a common view that “culture consists of some combination of artifacts (also called practices, expressive symbols, or forms), values and beliefs, and underlying assumptions that organizational members share about appropriate behavior” (Detert et al., 2000). Culture, therefore, is an explanatory variable that distinguishes one organization...
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...challenges to engineers and designers alike. Since the building can hold up to 35,000 people at once, it is essential that it is strong, comfortable and able to move people up and down it at a steady rate. This essay will explore how the designers and engineers went about solving these issues. One of the key problems the engineers had to overcome was effect of the wind load and how it would affect the building motions due to the extraordinary height of the tower. Wind load is something that must be taken into account for all buildings, but obviously the wind velocity increases the higher you go and since the structure is over 800 metres tall, there is guaranteed to be a large wind force acting on the building. Three different engineering firms: Skidmore, Owings and Merrill who were all working on the project, hired the RWDI (Rowan Williams Davies & Irwin Inc.) a wind and environmental engineering firm to conduct wind studies on the Burj Dubai’s design. The RWDI had worked on a number of previous projects such as the Petronas Towers and the Taipei 101 and its facilities included four boundary wind tunnels. Their job was to minimize the effects of the wind load and building motion of the tower. Wind around an extremely tall skyscraper can result in the wind load changing direction or force and can cause...
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...just take off from the ground and fly thousands of miles from place to place. How does it all work, do you ever wonder? Well obviously it’s not magic; it’s mainly because of aerodynamics. And when we talk about aerodynamics, it goes way beyond elevators, rudders, etc. Therefore we go to the depths of aerodynamics and its power to control a massive plane in the air. To be engineering in aerospace we need this extensive knowledge. In this report, you will learn about how an aircraft moves. The stability and control of the aircraft we also learn the factors influencing the static stability, the static margin and load factors. This report also gives us knowledge about the aircrafts control systems. | | | 1.1 | Motion of an aircraft | 4 | 1.2 | Degree of freedom | 4 | 2.1 | Static stability | 5 | 2.2 | Static margin | 5 | 2.3 | Dynamic stability | 6 | 3.1 | Stability in an aircraft | 6 | 3.2 | Longitudinal stability | 6 | 3.2.1 | Longitudinal dihedral | 7 | 3.3 | Lateral stability | 7 | 3.3.1 | Dihedral | 7 | 3.3.2 | Sweepback | 8 | 3.3.3 | Keel effect | 8 | 3.4. | Directional stability | 9 | 3.4.1 | sweepback | 9 | 4.1 | Load factor | 9 | 4.2 | Maneuver envelopes | 10 | 4.3 | Constraints on load factor | 10 | 4.4 | Load factors with respect to different maneuvers | 11 | 5.1 | Horizontal stabilizers | 12 | 5.2 | elevators | 12 | 6.1 | Vertical stabilizers | 13 | 6.2 | rudder | 13 | 7.1 | Role of swept back wing | 13 | 8.1 | Role...
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...REFERENCE DOCUMENTS A.3 BASIC DATA B. ConcepT B.1 charaCteristiCS OF THE BUILDING – ASSESSMENT OF THE PRESENT CONDITION B.2 EFFECT OF THE EXISTING BUILDING ON THE OVERALL DESIGN B.3 LAYOUT AND OPERATION DESIGN – THE OFFICE BUILDING B.4 architeCtURAL DESIGN B.5 TRAFFIC C. ConcepT – THE OFFICE BUILDING C.1 charaCteristiCS OF THE BUILDING – ASSESSMENT OF THE PRESENT CONDITION C.2 EFFECT OF THE EXISTING BUILDING ON THE OVERALL DESIGN C.3 LAOUT AND OPERATION DESIGN – THE OFFICE BUILDING C.4 architeCtURAL DESIGN C.5 TRAFFIC d. ConcepT – THE HOTEL BUILDING C.1 charaCteristiCS OF THE BUILDING – ASSESSMENT OF THE EXISTING CONDITION C.2 EFFECT OF THE EXISTING BUILDING ON THE OVERALL DESIGN C.3 LAOUT AND OPERATION DESIGN – HOTEL C.4 DESIGN C.5 TRAFFIC COVER REPORT 1 IdentifiCATION DATA Project: Location: Cadastre Area: Investor: Design Team: ……………………………. ……………………………. ……………………………. 2 LIST OF REFERENCE DOCUMENTS - elementary consultations with the investor - geodesic survey drawings – the existing condition - maps from IMIP 3 BASIC DATA Building A Area balance Lot area: Built-up area: Greenery: Compacted area: Total rough area of the over-ground floors Total rough area of the underground floors Total built-up space of the over-ground floors Total built-up space of the underground floors Office area: Apartments area: Retail area: Number of required parking lots...
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...cylindrical fuselage, a lower freight bay and upper passenger compartment, swept back wings and a tricycle undercarriage. Some argue that this form is the conclusion of evolution and that it simple demonstrates the limiting form of the idea. Others take the view that any form is only the product of the circumstances that produced it and if these change the evolutionary form will change and can be changed. The ideas presented here follow this path. Prompted by the pressures for environmental sensitivity some ideas focus on ways to make dramatic, or at least important, savings in the amount of fuel used by the world’s airliners. Previously dismissed contributions to economy of fossil fuel lie behind the thinking of several new technological concepts. 1. The glider-like airliner Gliders has very high aspect ratio wings. These low drag wings allow them to sustain altitude in the lightest of upward thermals (about 1 fpm) and thereby to carry out long distance flight on no fuel at all. Their glide ratio is extremely shallow – in the order of 1 in 55 compared with a typical airliner of 1 in 15 (B747). Powered gliders are somewhere between a conventional a/c and a glider. Their small engines can be used to gain or to sustain altitude and the consumption of fuel is still only small. The concept is for airliners with some of the characteristics of a powered glider. It would have high aspect ratio wings and be fitted with substantial engines for climb out but much less powerful than those...
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...The delta wing-canard design makes Gripen the most agile fighter for close combat scenarios. Gripen NG, the new version of Gripen C/D can be armed with METEOR, AMRAAM, IRIS-T and AIM-9 missiles. The new generation aircraft incorporates a multi-frequency data link, fully integrated avionic mission system, long range PS05 multimode radar and sensor fusion. The Saab JAS 39 Gripen is a light single-engine multirole fighter aircraft manufactured by the Swedish aerospace company Saab. The Gripen has a delta wing and canard configuration with relaxed stability design and fly-by-wire flight controls. It is powered by the Volvo RM12, and has a top speed of Mach 2. Later aircraft are modified for NATO interoperability standards and to undertake in-flight...
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...Effect of a Paper Plane’s different masses on its time on flight The following experiment (underneath) is to do with a paper plane and its mass and time of flight. Here is a chance to experiment with different masses of a paper plane to observe how it affects it’s time of flight. Research Question: How does the mass (g) of a paper plane affect the time (seconds) of its flight? Hypothesis: It is expected that, the more mass on the paper plane’s wings, the time of flight will decrease. This is because more mass; the faster gravity will pull it down. *Independent variable: Number of paperclips (amount of mass in grams) Dependent variable: The time of flight –measured in seconds. X Controlled variables: Throw it with the same force in each throw, and same angle of the throw. Materials: Stop watch 3 pieces of A4 paper to make paper planes 1 balance 12 paperclips Method: Make 3 ordinary paper planes from A4 sheet of paper Find someone who is willing to throw the paper plane for all the trials in the experiment. Take the paper plane and weigh it using the balance (weighing scale), to note down its mass. Find an open space for the plane to fly freely and take your planes there. Throw 1 paper plane from shoulder level and start the stop watch at the same time of the throw. Stop the stop watch the moment when the plane touches the ground. Record your data and repeat steps 4-6 four more times. For the second trial, add 1 paperclip to each wing...
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...Wrights brothers first flight on a handmade fixed-wing aircraft to the most technologically advanced aircraft in the world, the F-35 Lightning II Fighter jet. Despite their vast differences, these aircrafts have some things in common; they are run by major components and aerodynamics that make flying possible. The major components of an airplane and their functions are what make an aircraft fly into the air. An aircraft has five major components: fuselage, wings, landing gears, empennage, and power plants. The many complex parts of an aircraft and schematics are all responsible for making the aircraft design. In an effort to understand the design, it is imperative to break down the most common basic components to reflect how they work together to make an aircraft fly into the air. The fuselage is the part of an aircraft that is designed to carry cargo, equipment, people etc. Each major component is attached to the fuselage. The most common shape of a fuselage is a cylinder like tube that was designed to decrease drag and produce a little lift. The fuselage material is made of steel/aluminum. The different shapes are welded together to create the strength and bond it needs to hold together. The shaped pieces are called trusses ("Aircraft structure -," 2006). The fuselage also contains a cockpit which is the control room of the aircraft. All action and commands happen in that section of the plane. The wings of an aircraft are attached to each side of the fuselage...
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...GEAR SYSTEM (GENERAL, MAIN LG) | 3 | NOSE LANDING GEAR AND EMERGENCY GEAR EXTENSION | 5 | LANDING GEAR SYSTEM CONROLS AND INDICATORS | 7 | WHEEL AND BRAKES | 8 | ANTI SKID SYSTEM | 10 | NOSE WHEEL STEERING SYSTEM | 13 | AIR BRAKES | 14 | BOEING 747 LANDING GEAR SYSTEM (GENERAL, MAIN GEAR AND DOORS) | 15 | NOSE GEAR AND DOORS | 16 | LANDING GEAR EXTENSION AND RETRACTION, WHEEL AND BRAKES AND STEERING | 18 | POSITION AND WARNING | 19 | CONCLUSION AND REFERENCES | 20 | INTRODUCTION: The undercarriage or landing gear in aviation is the structure that supports an aircraft on the ground and allows it to taxi, takeoff and land. Typically wheels are used, but skids, skis, floats or a combination of these and other elements can be deployed, depending on the surface. Landing gear usually includes wheels equipped with shock absorbers for solid ground, but some aircraft are equipped with skis for snow or floats for water, and/or skids or pontoons(helicopters). The undercarriage is a relatively heavy part of the vehicle, it can be as much as 7% of the takeoff weight, but more typically is 4-5%. Gulfstream G200 Landing Gear System General The G200 has 4 main landing gear tires and two nose landing gear tires. The landing gear is tricycle type with two wheels on each gear strut. Each unit retracts into its’ own well and is fully covered by doors, mechanically connected to the landing gear. Landing...
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...attempt to discuss the basic aerodynamic principles of flight. It will be based on Module 3, Learning Objective 1: ‘For a typical aircraft, describe the functions of the structure and the flight controls. Apply aerodynamic principles to explain how flight controls control pitch, roll, and yaw’. It will also outline the basic control surfaces of an aircraft and the primary and secondary effects of each of them. In addition, it will also explore Bernoulli’s Principle and the forces acting on an aircraft in flight. Table of Contents Introduction5 Main Components of An Airplane 6 * Fuselage * Wings * Empennage The Wing and the Aerofoil7 Aerodynamics of Flight (Bernoulli’s Principle) 8 The Forces in Flight 9 * Lift * Thrust * Drag * Weight The 3 Axes of Rotations 10 * Longitudinal Axis * Lateral Axis * Vertical Axis Main Control Surfaces11 * Ailerons * Elevators * Rudders Secondary Effects of Control Surfaces12 Conclusion14 List of Figures Figure 1: The Magic of Flight 3 Figure 2: Main Components of an Airplane 4 Figure 3: The Wing And Aerofoil 5 Figure 4: Aerofoil Nomenclature 6 Figure 5: Bernoulli’s Principle 7 Figure 6: Forces on An Airplane in Flight 8 Figure 7: The 3 Axes of Rotation 9 Figure 8: 6 Degrees of Freedom 10 Figure 9: Control Surface: Ailerons 11 Figure 10: Control Surface: Elevators 11 Figure 11: Control Surface: Rudders 11 Introduction Figure 1: The Magic of Flight Man...
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...Lake Affect Snow And it’s Effect on Aviation BY: Perlisha Humphrey And Duane Johnson Imagine driving on high way U. S. 2 in the Upper peninsula of Northern Michigan just outside of Marquette, on a sunny winter day as the skies turn dark and ominous clouds build in the distance. Suddenly, a “wall of white” appears several hundred yards ahead and some of the heaviest snow you have ever seen obscures everything in your path. You inch forward through the blizzard until you arrive on the other side – where skies once again turn sunny. Anyone who lives in the Great Lakes region is familiar with this unique type of winter weather. This heavily localized snowfall, known as lake-effect snow, is most common from November to February. The winter weather phenomenon is capable of whiting out large sections of the Great Lakes region, from South Bend, Indiana, to Buffalo, New York. Towns and cities at higher elevations can expect even larger amounts of lake-effect snow. The Recipe for Lake-Effect Storms Lake-effect snow forms in the winter when cold air masses move over warmer lake waters. As the warm lake water heats the bottom layer of air, lake moisture evaporates into the cold air. Since warm air is lighter and less dense than cold air, it rises and begins to cool. The moisture that evaporates into the air condenses and forms clouds, and snow begins falling. This may seem like the recipe for whole world but due to the sheer size of the great lakes and the fact...
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...Military Technology Land Force Air And Missile Defence Dealing With The Complexities Of Future Warfighting Lieutenant Colonel Inger Lawes Abstract In the future, land force commanders will need to manage the use of airspace to enable multidimensional manoeuvre—coordinating joint and coalition assets and denying adversaries. Battlespace management, in an era of uninhabited and automated systems, is becoming increasingly complex. The author argues for the development of a ‘land force air and missile defence’ (LFAMD) to enhance friendly capability and defeat conventional and asymmetrical enemy manoeuvre. Introduction T he Australian Defence Force (ADF) Future Warfighting concept asserts that ‘the challenges of complex environments reinforce our view that warfare is multi-dimensional.’ 1 In future warfare, because of the presence of both conventional and asymmetric air threats, air and missile defence will become an essential capability in enabling the land force to conduct multi-dimensional manoeuvre. Australian Army Journal • Volume III, Number 2 • page 109 Military Technology • Lieutenant Colonel Inger Lawes The Future Land Operating Concept Complex Warfighting describes the contemporary operational environment in terms of defining characteristics such as complex physical, human and informational terrain and urban environments, increased threat diversity, diffusion and lethality. These characteristics necessarily impose a broader spectrum...
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