The Geographical Description Of Orlando

The Geographical Description Of Orlando State of Florida is located on the Gulf Coast in the south-eastern United States. It is bordered to the west by the Gulf of Mexico, to the north by Alabama and Georgia, and to the east by the Atlantic Ocean. Orlando is a major city in the central region of the U.S. state of Florida. The geography of Orlando is mostly wetlands, consisting of many lakes and swamps. The terrain is generally flat, making the land fairly low and wet. In the area there are hundreds of lakes and the largest one is Lake Apopka. Central Floridas bedrock is mostly limestone and very porous. The Orlando area is susceptible to sinkholes. Orlando International Airport is the busiest airport in Florida. Located 10.5km (6.5 miles) southeast of Orlando, the airport is served by more than fifty airlines. In the airport there are more than 100 retail shops, food and beverage outlets, and the airport is a self-contained environment with full service banking, currency exchange, salon and post office. Duration of the flight from Scotland can take between 11 18.5 hours, possibly with a connecting flight from London. The Rosen Inn is located west of the airport and the transfer time from the airport to the hotel is approximately 20 minutes. Local Time Zone Orlando is in the Eastern Time Zone and it is 5 hours behind of Greenwich Mean Time (GMT) during the Eastern Standard Time and 4 hours behind of GMT during Daylight Saving Time. In Orlando the Daylight Saving Time (DST) started on Sunday, 13 March and will end on Sunday, 6 November. Description of Tour Operator Virgin Tour Operator has won several awards such as British Travel Award in 2007 and it is named Best Tour Operator to USA/Canada. The company was voted by the customer and received its third Best Package Holiday Company Long Haul award. Virgin Tour Operator offers excellent holiday packages to Florida and everywhere around the world. Virgin Holidays is the largest, extremely popular, and most successful transatlantic tour operator, it beats rival operators such as Thomas Cook and Jetlife. Description of Selected Holiday Walt Disney World Seaworld Orlando Rosen Inn Hotel Epcot Universal Orlando Resort Orlando International AirportThe holiday I have chosen as it was requested is in Orlando. The hotel that I selected is located in International Drive, which is one of Orlandos most lively and dynamic areas and is right in the centre of some of the worlds most famous theme parks and attractions, including museums, mini-golf courses and restaurants ranging from fast food to gourmet cuisine. Its also a shoppers paradise with designer outlet stores, shops and boutiques. The area can be explored by foot or by jumping on the I-Ride Trolley which served all the attractions along international Drive. Rosen Inn Hotel Within the hotel guests can enjoy Plaza Garden Restaurant, Lite Bite Deli with a late opening, Zebras Sports Bar and Grille with entertainment and bar menu until midnight. The smoking area is open on the outdoor patio deck. Smooth Java Coffee Bar is featuring Starbucks premium coffee products, fresh fruit smoothies and a variety of pastries. Food is served until midnight. The hotel has three swimming pools, electronic games room and childrens playground. Car hiring with free parking and breakfast are also included. Pointe Orlando shopping complex is on the opposite side offering some great clothes shops and twenty-one cinema screens. Free scheduled shuttle takes guests to the best attractions of the International Drive area. Universal Orlando Resort is 10 minute, Walt Disney Resort is 20 minute and SeaWorld Orlando is 5 minutes away from the accommodation. Resort representatives are available 7 days. Room Information All rooms have two double beds, featuring pillow-topped mattresses, radio alarm clock, refrigerator, microwave, coffee maker, electronic safe, iron and ironing board, TV with free Disney Channel and Premium Movie Channel. In-room pay-cinema channels are also available and there is a complimentary wireless internet in the rooms and throughout public areas of hotel. Rooms are air-conditioned and non-smoking. Climate Orlando has a subtropical and very humid climate. The average annual temperature is a comfortable 72.4  °F (22.4  °C). Average annual rainfall amounts to over 50 inches per year, keeping central Florida lush and green throughout the year. Prevailing winds are southerly at 9 mph. The average elevation of the region is 127 feet above sea level. There are two major seasons each year: Hot and rainy, lasting from June until late September. During this time the temperatures can be uncomfortably hot. Dry, warm season, from October through May; bringing less frequent rainfall, yet still with warm temperatures. Occasionally night time temperatures can plunge surprisingly low. Thunderstorms are common between May and September and tend to be short but heavy, offering some respite from the heat. Summer is also hurricane season from June to November. Of course everything is air conditioned in Orlando, the theme parks sell inexpensive umbrellas and rain parkas, and there are the water parks. Summer travel to Orlando Florida is still fun and winter travel is wonderful. Theme Parks Universal Orlando Resort Intl Drive North Area This is another exciting full day activity. At this real, working film and TV production facility visitors can go behind the scenes and jump right into the action of their favourite movies. Visitants can plunge into darkness on the psychological thrill ride, Revenge of the Mummy; see, hear and feel the action through the miracle of OgreVision in Shrek 4, save the earth from aliens on the interactive ride MEN IN BLACK Alien Attack, or experience the Universals newest coaster Hollywood Rip Ride Rockit. Walt Disney World Resort Area At Disneys Hollywood Studios is one of the best in popular entertainment. Visitors can experience what it feels like to be on the stage as a star from their own adventure and share it as part of the Magical Gatherings experience. Walt Disney World Resort Area Disney storytelling comes to life in a kingdom where visitors can see real and imaginary animals, thrilling attractions, shows and the majesty of the nature. This is another excellent day out offering lots of fun, wonder and adventure. Discovery Cove SeaWorld International Drive South Area Discovery Cove is a day of adventure and a lifetime of memories. Visitors can swim with dolphins, wade with mysterious rays, snorkel among thousands of tropical fish, and safely come eye-to-eye with sharks and barracudas, hand-feed exotic birds. Families can relax on genuine beaches and enjoy an all-inclusive day of discovery. Universals Islands of Adventure Universal Orlando Resort Intl Drive North Area It is an adventurous full day visit where visitors can experience five uniquely themed islands such as Seuss Landing, The Lost Continent, Jurassic Park, Toon Lagoon and Marvel Super Hero Island. Excursionists can battle villains in 3-D on The Amazing Adventures of Spider-Man, defy gravity as The Incredible Hulk Coaster takes them on a high-speed roller coaster rampage, escape the jaws of a T-Rex on the Jurassic Park River Adventure, brave white-water rapids on Popeye Blutos Bilge-Rat Barges or take a spin through the mischievous world of The Cat in the Hat. As newness The Wizarding World of Harry Potter provides visitors with a one-of-a-kind experience complete with multiple themed attractions, shops and a restaurant. Walt Disney World Resort Area Epcot is another fantastic full day visit where families have to opportunity to see fascinating cultures and numerous wonders of the world through dazzling shows, interactive experiences and amazing attractions. SeaWorld Orlando SeaWorld International Drive South Area In SeaWorld Orlando is an adventurous full day theme park where families can encounter up-close animal experiences, unforgettable performances, and the next generation of thrills. SeaWorlds all-new killer whale show connects guests to the sea, and killer whales, with a new level of energy and excitement while it educates and inspires them to make a difference in this world. Visitors can feed sea lions or get on the flying roller coaster. Orlando helps vacation adventures become lifelong memories. There is an onsite restaurant offering good selection of food to all families. Other attractions Gatorland 14501 South Orange Blossom Trail, Orlando Gatorland is located around 6.5 miles from the hotel. It is a 110-acre theme park and wildlife preserve, combining Old Florida charm with exciting, new exhibits and entertainment. It provides affordable-priced family fun with thousands of alligators, crocodiles, a childrens water park, aviary, breeding marsh with observation tower, petting zoo, nature walk, educational wildlife programs, gift shop, Floridas best train-ride, restaurant, and much more. Central Florida Zoo Botanical Gardens 3755 NW US Highway 17/92, Sanford, It is located around 30 miles from the hotel. It boast over 400 animals, 23 acres of native gardens, an Insect Zoo and Reptile House, a childrens zoo with animals, ZOOm Air Aerial Adventures, a splash playground, live animal encounters and many educational opportunities and demonstrations. Lake Eola Park 195 N Rosalind Avenue, Orlando Lake Eola Park is popular destination in the downtown area with beautiful surroundings, ideal for walking. Other activities available to park visitors include renting swan-shaped paddle boats, electric gondola boats, feeding the live swans and other birds inhabiting the park. Dangers of the weather Key rules for coping with heat are to drink plenty of water to avoid dehydration and to slow down and cool off when feeling fatigued, a headache, a high pulse rate or shallow breathing. Overheating can cause serious, even life-threatening conditions such as heat stroke. Dangers of heat include: Heat cramps: Exercising in hot weather can lead to muscle cramps, especially in the legs, because of brief imbalances in body salts. Cramps become less frequent as a person becomes used to the heat. Heat syncope or fainting: Anyone not used to exercising in the heat can experience a quick drop in blood pressure that can lead to fainting. As with heat cramps, the cure is to take it easy. Heat exhaustion: Losing fluid and salt through perspiration or replacing them in an imbalanced way can lead to dizziness and weakness. Body temperature might rise, but not above 38.8 °C. In some cases victims should be hospitalized. Heat exhaustion is more likely after a few days of a heat wave than when one is just beginning. The best defence is to take it easy and drink plenty of water. Dont take salt tablets without consulting a physician. Sunstroke: In some cases extreme heat can upset the bodys thermostat, causing body temperature to rise to 40 °C or higher. Symptoms are lethargy, confusion and unconsciousness. Even a suspicion that someone might be suffering from sunstroke requires immediate medical aid. Sunstroke can kill. How to avoid? It is strongly recommended to protect eyes from the rays of the sun by wearing sunglasses or a wide brim hat when being outdoors for an extended period of time. Avoid staying in direct sunlight between 10 a.m. and 16 p.m. During that period is suggested to stay in the shades. Strong physical activities should be postponed to periods when the temperature is at normal level and not above the bearable limit. It is essential to protect the skin from UV rays by using sun creams with high SPF values or umbrella. Jet Lag Jet lag is the temporary disruption of the body clock when flying across several time zones. This causes the travellers internal clock to be out of sync with the external environment. Causes of Jet Lag When traveling across a number of time zones, the body clock goes out of sync with the destination time, and so it experiences daylight and darkness contrary to the rhythms it has grown accustomed to. The bodys natural pattern therefore becomes upset as the rhythms which dictate when the person should eat and sleep no longer correspond to the environment of the destination. Jet lag occurs, because the body cannot automatically realign these rhythms. The speed at which the body readjusts itself to new daylight and darkness hours and eating and sleeping patterns is entirely dependent upon the individual. So while it may take a few days for certain people to readjust to a new time zone, others seem to experience little disruption to their bodys natural sleeping pattern. The symptoms of jet lag can be quite varied such as fatigue, exhaustion, inability to sleep, disorientation, lost desire to eat, headaches, stomach aches and a general feeling of fuzziness. How to reduce? Taking shoes off to ease pressure on feet, blindfolds, ear plugs, neckrests and blow-up pillows are all useful in helping to get quality sleep while flying. Walking up and down the aisle, standing for spells, and doing small twisting and stretching exercises in the seat, all help to reduce discomfort, especially swelling of legs and feet. The dry air in aircraft causes dehydration. Drinking plenty of non-alcoholic fluids counters this. Water is better than coffee, tea and fruit juices. Get plenty of exercise in the days prior to departure and try to avoid sickness such as the flu, colds and so on. Amenities of the area Local transport I-RIDE Trolley bus system is the only that services on International Drive and it is very popular by tourists. The regional public bus system that operates in Central Florida is called LYNX. The bus stops can be recognised by either a pink bus or a paw symbol on a round sign. Standard bus fare is $2 per person one way, with free transfers and daily passes also can be bought on the vehicles for $4.50. Weekly passes need to be purchased in advance from the website or outlets in the area and they cost $16. In addition, LYNX also offers a free bus system within Downtown Orlando called LYMMO. If you plan on using LYNX it is strongly recommended that you visit the official website for route information: www.golynx.com or call 407-841-LYNX. Money In the U.S dollar system one dollar equals 100 cents. One British pound is worth about $1.62 but this amount can be changed depending on the daily exchange rate. Currency changing facilities can be found at the airport, and many places offers money exchange in the International Drive such as major banks or the Visitor Centre. Food and Drink Orlando is becoming one of the top gastronomic places; the city offers a wide range of cuisine from all over the world. There are more than 4000 restaurants, breakfast buffets, steakhouses and so on. There are full-service restaurants at every theme park. However, some areas like International Drive offer a high conception of dining outlets. Well-known chains can be found such as Hard Rock Cafà ©, Outback Steakhouse, Planet Hollywood etcetera. One of Orlandos main dishes is the traditional African gumbo, but Moroccan Cous cous can also be mentioned which is made of beef or chicken with vegetables, Dim sum which is fried bread stuffed with meat, vegetables or fruit; the Mofongo which is fried banana with pork cracklings and garlic; and many other fantastic options. Other information Culture Orlando is influenced by many different cultures. For example there are evident Portuguese and Spanish cultural influences; the languages are still spoken in Orlando. In the city cultural opportunities offer a mix of modern and traditional entertainment for tourists such as live orchestral music, opera and ballet. The city has two professional ballet companies. Museums, theatres and galleries are also great choices for visitors. There are many cultural events which acknowledge the rich ethnic background of the people of Orlando. The heritage of nature and wildlife is also very noticeable in Orlando and it is home to some beautiful parks, lakes and bird and animal sanctuaries. History Florida was named and discovered by Juan Ponce de Leon in 1513 while he was looking for the mythical Fountain of Youth and claimed it for Spain. Florida was held by England and Spain at different times and later, in 1819 it was eventually sold to the United States. Before Orlando was only known for its citrus industries, cattle and cotton. Nowadays it had become one of the most executive tourist destinations. Tipping Tipping can be confusing in any country. Normally the tip is given to the staff is 15 20 %. Service personnel who tipped are like bartenders, drivers on public transports, table servers at dining venues, or beauticians. Porters are traditionally tipped $1 per bag. Many restaurants already include tips on the bill for groups of six or more. Therefore, its better to ask the staff if the tip has already been added to the check. Souvenirs There are lots of shops in International Drive, most of them Chinese-owned, and they are offering gifts for cheaper price than Walt Disney stores or the shops in the theme parks. In the souvenir shops T-shirts, tags, jewellery, pyjamas, costumes and a lot more can be purchased. It is guaranteed that everyone finds something unique and nice.

Surface Pressure Measurements on an Aerofoil

DEN 302 Applied Aerodynamics SURFACE PRESSURE MEASUREMENTS ON AN AEROFOIL IN TRANSONIC FLOW Abstract The objective of this exercise is to measure the pressure distribution across the surface on an aerofoil in a wind tunnel. The aerofoil is tested under several different Mach numbers from subsonic to supercritical. The purpose of measuring the pressure distributions is to assess the validity of the Prandtl-Glauert law and to discuss the changing chracteristics of the flow as the Mach number increases from subsonic to transonic.As a result of the experiment and computation of data, the aerofoil was found to have a critical Mach number of M=0. 732. Below this freestream Mach number the Prandtl-Glauert law predicted results very successfully. However, above this value, the law completely breaks down. This was found to be the result of local regions of supersonic flow and local shockwaves. Contents Abstract2 Apparatus2 1. Induction Wind Tunnel with Transonic Test Section2 2. Aerofoil mode l3 3. Mercury manometer3 Procedure3 Theory3 Results4 Discussion8 Transonic Flow8 Analysis9 Conclusion11 Bibliography11Apparatus 1. Induction Wind Tunnel with Transonic Test Section The tunnel used in this experiment has a transonic test section with liners, which, after the contraction, remain nominally parallel bar a slight divergence to accommodate for boundary layer growth on the walls of the test section. The liners on the top and bottom are ventilated with longitudinal slots backed by plenum chambers to reduce interference and blockage as the Mach number increase to transonic speeds. The working section dimensions are 89mm(width)*178mm(height). The stagnation pressure , p0? is close to the atmospheric pressure of the lab and with only a small error ,is taken to be equal to the settling chamber pressure. The reference staticpressure, p? , is measured via a pressure tapping in the floor of the working section, well upstream of the model so as to reduce the disturbance due to the model. The ‘freestream’ Mach number, M? , can be calculated by the ratio of static to stagnation pressure. The tunnel airspeed is controlled by varying the pressure of the injected air, with the highest Mach number that can be achieved by the tunnel being 0. 88. 2. Aerofoil modelThe model used is untapered and unswept, having the NACA 0012 symmetric section. The model chord length, c, is 90mm and the model has a maximum chord/thickness ratio of 12%. Non-dimensionalised co-ordinates of the aerofoil model are given in table 1 below. Pressure tappings, 1-8 , are placed along the upper surface of the model at the positions detailed in table 1. An additional tapping, 3a, is placed on the lower surface of the aerofoil at the same chordwise position as tapping 3. The reason for including the tapping on the lower surface is so that the model can be set at zero incidence by equalizing the pressures at 3 and 3a 3.Mercury manometer A multitube mercury manometer is used to record t he measurements from the tappings on the surface of the model. The manometer has a ‘locking’ mechanism which allows the mercury levels to be ‘frozen’ so that readings can be taken after the flow has stopped. This is useful as the wind tunnel is noisy. The slope of the manometer is 45 degrees. Procedure The atmospheric pressure is first recorded, pat, in inches of mercury. For a range of injected pressures, Pj, from 20 to 120Psi, the manometer readings are recorded for stagnation pressure (I0? , reference static pressure (I? ), and surface pressure form tappings on the model (In, for n=1-8 and 3a). Theory These equations are used in order to interpret and discuss the raw results achieved from the experiment. To convert a reading, I, from the mercury manometer into an absolute pressure, p, the following is used: p=pat ±l-latsin? (1) For isentropic flow of a perfect gas with ? =1. 4, the freestream Mach number,M? , is related to the ratio between the static and stagnation pressures by the equation: M? =2? -1p? p0? -? -1? -1. 0(2) Pressure coefficient, Cp , is given by:Cp=p-p? 12 U? 2(3) For compressible flow this can be rewritten as: Cp=2? M? 2pp? -1(4) The Prandtl-Glauert law states that the pressure coefficient, CPe, at a point on an aerofoil in compressible, sub-critical flow is related to the pressure coefficient, CPi, at the same point in in incompressible flow by the equation: CPe=CPi1-M? 2(5) Due to its basis in on thin aerofoil theory, this equation does not provide an exact solution. However it is deemed reasonably accurate for cases such as this in which thin aerofoils are tested at small incidence.The law does not hold in super-critical flow when local regions of supersonic flow and shockwaves appear. The value of the critical pressure coefficient, Cp*, according to local sonic conditions is calculated by: Cp*=10. 7M? 25+M? 263. 5-1for? =7/5(6) The co-ordinates for the NACA 0012 section are as follows: Figure 1-Co-ordinates for aerofoil (Motallebi, 2012) Results Given atmospheric conditions of: Patm=30. 65 in-Hg Tatm=21 °C The following results were achieved: Figure 2-Pressure coefficient vs x/c for M=0. 83566 Figure 3-Pressure coefficient vs x/c for M=0. 3119 Figure 4-Pressure coefficient vs x/c for M=0. 79367 Figure 5-Pressure coefficient vs x/c for M=0. 71798 Figure 6-Pressure coefficient vs x/c for M=0. 59547 Figure 7-Pressure coefficient vs x/c for M=0. 44456 Figure 8-Cp* and Cpminvs Mach Number From figure 7 the critical Mach number is able to be determined. The critical Mach number (the maximum velocity than can be achieved before local shock conditions arise) occurs at the point where the curves for Cp* and Cpmin cross. From figure 7 we can see that this value is, M? =0. 732. Discussion Transonic FlowTransonic flow occurs when ‘there is mixed sub and supersonic local flow in the same flow field. ’ (Mason, 2006) This generally occurs when free-stream Mach number is in the range of M=0. 7-1. 2. The local region of supersonic flow is generally ‘terminated’ by a normal shockwave resulting in the flow slowing down to subsonic speeds. Figure 8 below shows the typical progression of shockwaves as Mach number increases. At some critical Mach number (0. 72 in the case of Figure 8), the flow becomes sonic at a single point on the upper surface of the aerofoil.This point is where the flow reaches its highest local velocity. As seen in the figure, increasing the Mach number further, results in the development of an area of supersonic flow. Increasing the Mach number further again then moves the shockwave toward the trailing edge of the aerofoil and a normal shockwave will develop on the lower surface of the aerofoil. As seen in figure 8, approaching very close to Mach 1, the shockwaves move to the trailing edge of the aerofoil. For M>1, the flow behaves as expected for supersonic flow with a shockwave forming at the leading edge of the aerofoil.Figure 9-Pr ogression of shockwaves with increasing Mach number (H. H. Hurt, 1965) In normal subsonic flow, the drag is composed of 3 components-skin friction drag, pressure drag and induced drag. The drag in transonic is markedly increased due to changes to the pressure distribution. This increased drag encountered at transonic Mach numbers is known as wave drag. The wave drag is attributed to the formation of local shockwaves and the general instability of the flow. This drag increases at what is known as the drag divergence number (Mason, 2006).Once the transonic range is passed and true supersonic flow is achieved the drag decreases. Analysis From figure 7, the conclusion was reached that the critical Mach number was 0. 732. This means ultimately that in the experiment local shockwaves should be experienced somewhere along the aerofoil for Mach numbers M=0. 83566, 0. 83119 and 0. 79367. According to transonic theory, these shockwaves should be moving further along the length of the aerofoil as the freestream Mach number increases. To determine the approximate position of the shockwaves it is useful to look again at equation (4).Cp=2? M? 2pp? -1 Assuming constant p? , as static pressure in the test section is assumed to be constant and constant free stream Mach number as well, equation (4) may be written as: Cp=const. pconst. -1 Normal shockwaves usually present themselves as discontinuous data, particularly in stagnation pressure where there is a large drop. To detect the rough position of the shockwave on the aerofoil surface it is useful to look at the detected pressure by the different tappings and scrutinize the –Cpvs x/c graph to see where the drop in pressure occurs.Investigating the graphs for the supercritical Mach numbers yields these approximate positions: M| x/c, %| 0. 835661| 40-60| 0. 831199| 35-55| 0. 793676| 25-45| Figure 10- Table showing approximate position of shockwave According to the theory described earlier, these results are correct as it demonstrates the shockwave moving further along the aerofoil as the Mach number increases. As seen in figure 8, given a sufficiently high Mach number, a shock may also occur on the lower surface of the wing. This can be seen for M=0. 835661, in figure 1, where there is a marked difference in pressure between tappings 3 and 3a.The theoretical curves on each –Cpvs x/c graph were designed using the Prandtl-Glauert law. As mentioned earlier, this law is based on thin aerofoil theory, meaning it is not exact and there are sometimes large errors between the proposed theoretical values and the experimental values achieved. These large errors are seen most clearly in the higher Mach numbers. This is because in the transonic range, where there is a mixture of sub and supersonic flow, local shockwaves occur and the theoretical curves do not take shockwaves into account.Hence, the theory breaks down when the freestream Mach number exceeds the critical Mach number for the aerofoil. At l ower Mach numbers, the theoretical values line up reasonably well with those achieved through experiment. There only seems to be some error between the two, mainly arising in the 15-25% range. However, overall the Prandtl-Glauert law seems to be reasonably accurate as long as the Mach number remains sub-critical. The experiment itself was successful. The rough position of the shockwave and the critical Mach number were able to be identified.There are however some sources of inaccuracy or error that can be addressed of the experiment is to be repeated for ‘bettter’ results. Aside from the normal human errors made during experimentation the apparatus itself could be improved. Pressure tapping 1 (the closest to the leading edge) and pressure tapping 8 (the closest to the trailing edge) were placed at 6. 5% and 75% respectively. What this means is that they are not centralized relative to the leading and trailing edge effectively meaning it is not able to be determined whet her or not the pressure is conserved.At a zero angle of incidence, the pressure at the tip of the leading edge should be equal to the pressure at the tip of the trailing edge. To improve this pressure tappings should exist at the LE and TE and possibly more pressure tappings across the aerofoil surface to provide more points for recording. Another source of improvement could be using a larger test section so that there is absolutely no disturbance in measuring the static pressure. However, this may only produce a minute difference in the data and may not be worthwhile for such little gain. ConclusionAs desired, a symmetric aerofoil was tested in transonic flow and the experimental results were compared to the theoretical values predicted by the PrandtlGlauert law. In the cases where there was a large disparity between experimental and theoretical results, an explanation was given, relying on the theory behind transonic flow. Bibliography H. H. Hurt, J. (1965). Aerodynamics for Naval Aviators. Naval Air Systems Command. Mason. (2006). Transonic aerodynamics of airfoils and wings. Virginia Tech. Motallebi. (2012). Surface Pressure Measurements on an Aerofoil in Transonic Flow. London: Queen Mary University of London.

English vs. Spanish Colonization Essay

From 1500 to 1700, the English colonization of the Chesapeake region and the Spanish colonization of the Central/South American region varied greatly in their primary motivations for settlement and the lasting effects imprinted into both societies. The English motives in settling the Chesapeake region were more economically-based, seeking greater economic opportunity and employment, while the Spanish effort took on a more religious approach that ended up having long-term effects on the way their culture and society developed. The effects both colonies felt differed in many ways, primarily due to the varying motivational influences felt by the English and the Spanish. However, similarities in colonial motivations and cultural impacts were present between both societies. English colonization of the Chesapeake region revolved around economic gain and opportunity that colonizers believed could be found in the New World. Overcrowding in England led to a desire for expansion and better emp loyment options for English settlers. Rumors of gold discovery in the New World also spurred an intense frenzy that English colonizers sought to pursue, resulting in the development of societies poorly suited for colonial life when gold was never found. On the other hand, Spanish colonization of Central and South America began with the Spanish conquistadors, who used the saying â€Å"God, Gold, and Glory† to describe their motivations for colonization. The dominant motivational force for the Spanish was the religious aspect, where conquistadors sought to spread Christianity throughout Central and South America. The â€Å"Glory† prospect was heightened by the yearning for Spain’s dominance over the Western Hemisphere, which was thought to be obtained through unifying native peoples through Bailey Kargo! IB HOTA 3rd period the Christian religion. Similar to one aspect of English motivations, the Spanish also sought to find gold and riches that they thought the New World had to offer. When Christopher Colombus returned from his expedition to the New World, he reported to the Spanish crown his confidence in the quest for wealth in this new land. He described his encounters with the natives where they traded him gold for various items, and even claimed he saw gold in the rivers. This fueled the Spanish obsession in their ultimate quest for wealth and riches. The effects of settling the Chesapeake region reflected the English economic motivations for colonization there. When the Jamestown Colony was founded in 1607, settlers found themselves ill-prepared for establishing a structured colony, especially when they were solely prepared for discovering gold. The Jamestown Colony struggled immensely at first due to lack of supplies and skills needed to create the foundations of a colonial society. However, John Rolfe’s introduction of tobacco to the region completely transformed the economy and played a key role in saving the Jamestown colony. Tobacco became a booming industry and plantation owners needed more workers for cheap labor. As a result, African slaves were introduced into the population to meet these needs, stimulating a new industry: the slave trade. The successful tobacco economy was also capable of financing the importation of indentured servants, which also played a major role in the labor force and became an integral part of the Chesapeake’s economy. Wealthy landowners were now able to have more help on their plantations and have access to more land, while servants now had the ability to own land and create a name for themselves among the colonies. Unlike English colonization, Spanish colonization in the Americas completely decimated native populations. The introduction of European diseases, particularly smallpox, along with Bailey Kargo! IB HOTA 3rd period updated European weaponry decimated Indian culture and transformed their way of life due to lack of immunity to such diseases and more primitive weapons. Native populations were seen as much weaker compared to the conquistadors and their armies, making them extremely easy to conquer. A cultural angle unique to the Spanish settlements was the creation of the Mestizo culture. Unlike the English, the Spanish conquerors and Native Americans intermarried, allowing for a completely new race to develop and contribute to society. Although they were regarded as lesser than other races and looked down upon, the creation of the Mestizo culture proved to become a unique impact of Spanish colonization that later English settlers chose not to conform to. The introduction of the encomienda system was also a significant effect that became an integral part of Spanish society. When the Spanish conquered natives, these natives were required to perform work for Spanish landowners. In return, the natives would receive protection from other tribes and the conversion to the Christian faith. This system was extremely beneficial to the colonists who received land and gained Christian converts, but many native tribes were reduced to involuntary servitude that further devastated Indian populations in addition to disease and war. The differing motivations behind English colonization of the Chesapeake region and the Spanish of Latin America proved to directly affect the way each colonies were formed from 1500 to 1700. English colonization revolved around a more economic basis, while the Spanish focused more on religious aspects that managed to integrate their way into its economy as well. Despite these differences, both societies found a common motivation in the search for gold and riches, and both incorporated different forms of slavery, indentured servitude and African slaves in the Chesapeake and the encomienda system in Latin America, into their economies that stimulated Bailey Kargo! IB HOTA 3rd period each colony’s development. The growth and expansion of both colonization efforts eventually would fuel the newfound desire of other European nations to join the race to the Americas in an attempt to assert their dominance and further diversify societies of the New World.

COMM292 Case Studies - 23202 Words

1. University of British Columbia Principles of Organizational Behaviour Girish Ananthanarayana COMM 329 - Section 202 - Winter Term 2 2014-15 Principles of Organizational Behaviour Girish Ananthanarayana COMM 329 - Section 202 - Winter Term 2 2014-15 University of British Columbia Table of Contents Teamwork Turmoil............................................................................................................................5 Campbell and Bailyns Boston Office: Managing the Reorganization.............................................13 The Rise of President Barack Hussein Obama..............................................................................23 2. TEAMWORK TURMOIL Tony Marshall, a second-year learning†¦show more content†¦UVA-OB-0897 UVA-OB-0897 received a dual undergraduate degree in finance and information systems. Prior to business school, she worked as an analyst for a private foundation. Martin planned to focus her career on private wealth. Despite the great amount of networking that her chosen career path required, Martin was very involved in the school community. She spent a lot of time working on projects for the Black Business Student Forum and the National Association of Women MBAs. Daren Onyealisi was originally from Nigeria and had been living in the United States for more than 10 years. He graduated from the University of Maryland with a degree in government. Following his undergraduate degree, Onyealisi worked as a policy research analyst for the District of Columbia, then changed career paths and worked as a real estate analyst for three years before attending business school. Onyealisi was a first-generation college graduate and awarded the Robert Toigo Foundation Fellowship upon entering the MBA program.1 While Onyealisi was not very involved in the graduate school community, through the Big Brothers Big Sisters of America organization he was a Big Brother for local youths. Onyealisi planned to target the consulting industry for his summer internship. Rob Delery was the only scientist in the group and earned a BS in chemical engineering from Penn State. During his undergraduate years, Delery was a member of the Penn