The Fish by Elizabeth Bishop Essays -- elizabeth bishop poem poetry fi

The Fish by Elizabeth Bishop      With less than fifty distributed sonnets Elizabeth Bishop isn't one of the most conspicuous writers within recent memory. She is anyway notable for her utilization of symbolism and her capacity to pass on the narrator?s feelings to the peruser. In her clearly visual sonnet 'The Fish', the peruser is presented to a story wherein the utilization of language brings the peruser into the story as well as aims the pictures to rise above the composed work. In the sonnet, Bishop utilizes various abstract gadgets, for example, analogies, descriptors, and distinct language. These gadgets finish in the peruser encountering an exact and itemized mental picture of the sonnet's setting and happenings.      One of the most pervasive of the abstract apparatuses utilized in this sonnet is the analogy. Over and over all through the sonnet Bishop utilizes the analogy to give the peruser a more clear image of the current circumstance. The metaphor is a perfect abstract apparatus to utilize when the creator is attempting to pass on a tactile depiction of an item or thought. While portraying the fish?s physical appearance in lines 9-15 she thinks about the fish?s skin to ?antiquated backdrop?; this promptly gives the peruser an impression of the age and outward appearance of the fish. Later in the sonnet when in lines 61-62 she portrays the bits of broken angling line dangling from the fish?s mouth as ?decorations with their strips/frayed and faltering? she is utilizing a likeness to give the impression of pride and respect. This comes at a moment that ...

Human Resource Issues in India, China, Brazil, and Nigeria Essay

Human Resource Issues in India, China, Brazil, and Nigeria - Essay Example The paper tells that in all the four nations that were examined, the work showcase is huge, and an open door for the organization to extend its business. The change to late models of HR is a key solidarity to the countries and this will impact decidedly to the organization. Culture is a major danger to the foundation of the organization, and this is a direct result of the affectability of the issues being tended to. One shortcoming of these countries is the high turnover as seen in India. It is suggested that the organization exploit the huge work advertise. Be that as it may, it ought to know about the current social and policy driven issues in these countries. These issues represent a genuine test to the foundation and development of the organization. HR are viewed as the most pivotal resource of any association; be that as it may, not all associations are able to do completely saddling its latent capacity. The human asset framework is characterized as a lot of individual however i nterrelated procedures, exercises, and capacities that are planned for keeping up, creating or drawing in a company’s HR. So as to upgrade operational execution, there is the need to similarly deal with the framework in both assembling and administration associations. Inventive assembling rehearses and modern innovations do almost no to improve operational execution except if the basic HRM (human asset the executives) rehearses are set up to make a consistent socio-specialized framework. Consequently, there is a requirement for associations to evaluate their current practices in HRM and correct if necessary so that representatives can productively add to the improvement of operational execution. There has been an extensive move towards acknowledging HR in the Indian associations. This is on the grounds that they have become methodology driven rather than business as usual, which is induced by culture.

POLICY MEMO PAPER ON DOMESTIC POVERTY Research Example | Topics and Well Written Essays - 1750 words

Strategy MEMO ON DOMESTIC POVERTY - Research Paper Example In this manner, moderates accept that the answers for the United States neediness level records ought to underscore more on higher relationships rates, moral obligation, and less births without any father present. In any case, on the opposite side, dissidents accept that the answers for the neediness level files in the United States can be tended to by concentrating consideration on the negative effects of cutting government spending plans for against destitution programs, the requirement for establishing youth improvement programs and tending to the negative impacts of demonstrating charge reliefs to the rich. As per report from the Bread for the World Institute about 12.9% of individuals in the United states are poor, suggesting that 1/8 individuals you run over in the United States at any rate one is poor. What's more, the report further expresses that about 12.1% are likewise food shaky, once in a while alluded to us â€Å"at danger of hunger† Therefore, it's anything but a fortuitous event that food and destitution rates are at similar levels. Consequently, this is a clear ramifications that the in spite of the broad of the 1990s government assistance changes and the ongoing year’s monetary development in the United States, local destitution despite everything stays a major test (Melissa and Benjamin, 2014). The idea of government assistance changes in the U.S. is anything but another thought. The Federal government has been liable for subsidizing low-pay Americans’ appropriation programs in the previous years with the point of lessening neediness to empower low-pay families achieve independence through for example TANF program (Office of Family Assistance, 1999). For example, a portion of the targets of the TANF program are: Cursorily, the targets previously mentioned appear not be upholding for the changeless remain of the low pay workers in the government assistance programs, however with the commencement of the government assistance programs by the Federal government, the issue of neediness has exacerbated throughout the years paying little mind to the accomplishments made financially. Hence, the inclusion of

Special Friendship Essay Research Paper I walked free essay sample

Specific Friendship Essay, Research Paper I strolled place from school, shipping a substantial weight of books on my stinging shoulders. Each measure I took was went with a desire that I was at that point at place, laying on my comfortable bed. I strolled on, my eyes stuck on the consumed dark course. As I hauled my pes along, I could see little bits of dried pitch turn overing on the unsmooth surface. After creation my doorsill, I hurled an overwhelming suspiration of calm and pleasance. Finally, I have arrived at my since quite a while ago held up finish ; place. My rosy, gluey thenar connected for the doorhandle. I was around to put pes onto the cool sparkling tiles when I heard a delicate whimper fighting against eminent loss me. At the point when I went to search for the start of the sound, I felt something rage coppice past my mortise joint. Looking down at the anger thing, I was attached to the land. We will compose a custom exposition test on Exceptional Friendship Essay Research Paper I strolled or on the other hand any comparable point explicitly for you Don't WasteYour Time Recruit WRITER Just 13.90/page Directly at that place, glancing back at me, was a lovely dark kitty. I could non accept my eyes. Before I could even accept of what to make straightaway, the kitty ran into the kitchen. At that point, I heard my male parent blast in torment. I was given a 10 proceedingss address. In spite of the fact that I clarified that the cat went into the house when I came place, my male parent obstinately accompanied the choice that I deliberately let it in. After the talk, I was requested to toss the kitty out of the house. Hesitantly, I carried it to a hotel territory close my home. I had brought along a Sn of pilchards, which I took without anyone? s comprehension. I gave the kitty the pilchards and watched it eat up it. I stroked the delicate, smooth wrath creature and said farewell, go forthing it behind. Shockingly, the kitty ever hangs tight for me at my doorsill when I come back from school. It did non travel into my home yet then again stood by persistently for me to adjust into my insouciant array before passing on it to the hotel territory with a Sn of feline supplement that has cost a one-fourth of my school disbursals. This continued for the accompanying two hebdomads, and the accompanying and the accompanying. The kitty has so become my companion, a specific companion. Now and again, when I am really pressurized with my school task, I will kick to the kitty. People groups may trust I am crazy or simply clearly idiotic. In any case, I figure I made the best decision. This is on the grounds that by making so I can truly encounter the power per unit zone inside me go forthing, everytime I grumbled to the kitty. Moreover, the kitty appears to get me. It would cream my guardianships thus energetically seize with teeth my fingers. It resembled expressing me to cheer up. This specific agreeable relationship went on. The kitty is presently a full, solid feline. I do non see it commonplace yet I will neer cover to go forward supplement for it at my doorsill. This specific inviting relationship is so an encounter I am really pleased with.

How Personality Traits Can Influence Depression in Kids

How Personality Traits Can Influence Depression in Kids Depression Childhood Depression Print How Personality Traits Can Influence Depression in Kids By Lauren DiMaria linkedin Lauren DiMaria is a member of the Society of Clinical Research Associates and childhood psychology expert. Learn about our editorial policy Lauren DiMaria Medically reviewed by Medically reviewed by Steven Gans, MD on August 05, 2016 Steven Gans, MD is board-certified in psychiatry and is an active supervisor, teacher, and mentor at Massachusetts General Hospital. Learn about our Medical Review Board Steven Gans, MD Updated on February 03, 2020 Depression Overview Types Symptoms Causes & Risk Factors Diagnosis Treatment Coping ADA & Your Rights Depression in Kids Gary John Norman / Getty Images When it comes to your own child, understanding the differences between a personality trait and a mood state can be a bit confusing, especially if your child has a mood disorder like depression. Studies have also shown that there is a relationship between personality traits and depression. Overview Here we take a look at the definitions of personality trait, mood state, and depression so you can better understand your child, identify the signs of depression, and get the mental health help they need. What Is a Personality Trait? A personality trait is a stable or relatively unchanging characteristic that identifies individual differences in people. For example, if your child has bipolar disorder, they may have the personality trait of impulsiveness. This is a personality characteristic that impacts a persons reactions to events. Trait impulsivity does not change much over time or between bipolar (manic and depressive) and normal phases. Another example is your child being stubborn, loving, or independent. Those are all personality traits that they were born with. While they may change a bit as your child develops, they are ultimately traits that make your child who they are. What Is a Mood State? A mood state is a temporary way of being or feeling that affects our overall well-being and mental health. For example, if your child has major depressive disorder, they may feel very sad for several weeks at a time. This sad mood is a temporary mood state and not a part of their personality makeup. A sad mood can be improved with treatment. What Is Depression? Depression is a complex mood disorder with both biological and social causes connecting the mind and body. The symptoms of depression, which in children can include irritability, anger, defiant anger, declining grades, and physical complaints, are persistent and interfere with daily functioning. Depression is treatable, often with a combination of medication, therapy, and lifestyle changes. What Parents Should Know About Childhood Depression The Relationship of Personality to Depression Studies show that people with certain personality traits are more susceptible to depression, which potentially means that screening for depression in children could be easier since traits are easy to assess. A review published in the Annual Review of Clinical Psychology that looked at how personality traits influence depression showed how much they affect both outlook and the development of depression.?? Specific traits that are linked with depression include: Neuroticism/negative emotionality: Sadness, moodiness, instability, and anxietyExtraversion/positive emotionality: Sociability, talkativeness, expressiveness, and excitabilityConscientiousness: How thoughtful and organized a person is (or isnt) The neuroticism/negative emotionality trait accompanied by a depressive personality was particularly predictive of depression developing in the future, according to the researchers. In fact, a separate study of teenagers published in the Clinical Psychological Science found that teens who score high on the personality trait of neuroticism are also more likely to develop depression as well as anxiety.?? Do Personality Traits Predict Depression? Researchers also found that factors like genetics and environment play a role in personality traits influencing depression. And personality trait risk factors are evident from an early age. So what does this mean? Well, young children who are at risk could be identified early and personality traits may predict and influence the course and treatment response of depression, say researchers. The study also noted that while personality traits influencing depression may differ depending on the kind of depressive disorder, they play an especially important role in early-onset, chronic, and recurrent depressive conditions. Further research needs to be done, particularly on the role personality traits play in other depressive disorders, not just major depression, as well as how this impacts young children. If You Have Concerns Researchers and clinicians have developed  standardized tests  for assessing personality traits and temporary mood states. If you have concerns about your childs personality traits or moods, talk to their pediatrician or mental health professional. Since most children wont be able to articulate their emotions, its also helpful for you to learn the symptoms of depression. Not every child who is depressed will experience the same symptoms; it may depend on their personality traits and mood states as well as the severity of their depression. In general, however, warning signs of depression in children fall into four categories: Emotional signs: Sadness, loss of pleasure or interest, turmoil, anxietyCognitive signs: Problems concentrating, pessimism, hopelessness, worthlessnessPhysical complaints: Changes in appetite, sleep patterns, headaches, stomachaches, sluggishnessBehavioral changes: Avoidance, withdrawal, clingy, demanding, restless, self-harm How to Spot Depression in a Child

Aircraft Electrical Systems Engine Performance Coursework - 1375 Words

Aircraft Electrical Systems Engine Performance (Coursework Sample) Content: AIRCRAFT ELECTRICAL AND MECHANICAL SYSTEMS: CASE STUDY AIRCRAFT ELECTRICAL SYSTEMS ENGINE PERFORMANCE(Student Name)(Course No.)(Lecturer)(University)(City State)(Date) Task 1Name of SectionExit Duct Area(Se)Exit Pressure (pe)Exit Air Velocity (Ve)Air Mass Flow ( QUOTE

) Aircraft Velocity (V0)Compressor200100350275200Diffuser220120300275200Combustion Chamber500110250275200Turbine40025900275200Exhaust60025700275200Propelling Nozzle3246.51080275200Average64.42596.67275200The thrust equation for a turbojet engine can be derived from Newtons Second law of motion, which implies that force equals the time rate of change of momentum.F =  QUOTE

For a Turbojet Engine, the Net thrust (FN) is normally given by the difference between the Gross thrust (FG) and the Momentum drug (Vinh, 1995). This is given as;FN = FG momentum drag = momentum thrust + pressure thrust momentum drug =  QUOTE

Ve + (pe po) Se -  QUOTE

Vo =  QUOTE

 (Ve Vo) + (pe po) Se = 275(596.67 200) + (64.42 1)324 = 109084.25 + 20548.08 = 129,632.33Where; W = is weight flow rate of the air passing through the engine. Ve = jet stream velocity pe = static pressure across propelling nozzle po = atmospheric pressure (given as 1 atm)Se = propelling nozzle area Vo = aircraft speed Thrust Shaft Horsepower for the turbojet engine will be given by the equation; thp =  QUOTE

 = bhpÆÅ ¾p= = 47,139Where; T = Thrust (lb)Vo = Velocity (ft/s)bhp = Engine break horsepower550 = conversion factor from ft-lbs to horsepowerÆÅ ¾p = propeller efficiencyPropulsive efficiency (ÆÅ ¾p) for the turbojet will be given by the equation;Èp = = = = = 0.5025Where; = Propulsive power output (thrust power given as FTV0) = Mechanical power input = Flight Velocity = Exit VelocityThe solution of Èp 1; this shows that not the entire mechanical power () goes into propelling the turbojet. Some of it is left as excess kinetic energy.Thermal efficiency (ÆÅ ¾th) for the turbojet engine will be given by the equation;ÆÅ ¾th = Where; m = Mechanical power i = Input energyIn order to find we use the formulae Èp =  QUOTE

 But we know that  QUOTE

 = FTV0 Therefore;  QUOTE

 = 129,632.33 x 200 = 25,926,466 Making  QUOTE

 the subject we have;  QUOTE

 =  QUOTE

 =  QUOTE

 = 51,594,957 Input energy  QUOTE

is given by; (fuel mass flow rate) x (fuel energy density) Therefore;  QUOTE

 = 275 x 2500 = 687,500lbs/hr In to BTU = 687,500 x 18,730 = 128768750 Èth = = 0.4006Overall efficiency (È0) for the turbojet engine will be given by the equation;È0 = = = Where; = the rate of energy input needed to generate the thrust = Propulsive power output (thrust power given as FTV0)Therefore; from the definitions of thermal and propulsive efficiency, the overall efficiency can also be given as;È0 = Èth x Èp È0 = 0. 4006 x 0.5025 = 0.2013Task 2Name of SectionExit Duct AreaExit Pressure (pe)Exit Air Velocity (Ve)Air Mass Flow ( QUOTE

) Aircraft Velocity (V0)Compressor20010035055200Diffuser22012030055200Combustion Chamber50011025055200Turbine4002590055200Exhaust6002570055200Propelling Nozzle3246.5108055200Fan90030500220900The thrust produced by turbofan engine is given by the equation;FN = FG momentum drag = momentum thrust + pressure thrust momentum drug =  QUOTE

Ve + (pe po) Se -  QUOTE

Vo =  QUOTE

 (Ve Vo) + (pe po) Se = 220(500-900) + (30-1)900 = 88000 + 26100 = 114,100Where; W = is weight flow rate of the air passing through the engine. Ve = jet stream velocity pe = static pressure across propelling nozzle po = atmospheric pressure Se = propelling fan area Vo = aircraft speedThrust Shaft Horsepower for the turbofan engine will be given by the equation; thp =  QUOTE

 = bhpÆÅ ¾p= = 186,70 9Where; T = Thrust (lb)Vo = Velocity (ft/s)bhp = Engine break horsepower550 = conversion factor from ft-lbs to horsepowerÆÅ ¾p = propeller efficiencyPropulsive efficiency (ÆÅ ¾p) for the turbofan engine will be given by the equation;Èp = = = = 1.285Where; = Flight Velocity = Exit VelocityThermal efficiency (ÆÅ ¾th) for the turbofan engine will be given by the equation;ÆÅ ¾th = Where; m = Mechanical power i = Input energyIn order to find we use the formulae Èp = But we know that = FTV0 Therefore;
 = 114,100 x 900 = 102,690,000 Making  QUOTE

 the subject we have;  QUOTE

 =  QUOTE

 =  QUOTE

 = 79,914,396 Input energy  QUOTE

is given by; (fuel mass flow rate) x (fuel energy density) Therefore;  QUOTE

 = 220 x 2500 = 550,000lbs/hr In to BTU = 550,000 x 18,730 = 103,015,000  QUOTE

 Èth = HYPER13 QUOTE HYPER14 = 0.7757Overall efficiency (È0) for the turbofan engine will be given by the equation;È0 = ÃƒË †th x Èp È0 = 0.7757 x 1.285 = 0.9968Task 3Name of SectionExit Duct AreaExit Pressure (pe)Exit Air Velocity (Ve)Air Mass Flow ( QUOTE

) Aircraft Velocity (V0)Compressor200100350275200Diffuser220120300275200Combustion Chamber500110250275200Turbine400251000275200Exhaust60025700275200Propelling Nozzle3246.51500275200Average64.42683.33275200The thrust produced by a modified turbojet engine is given by the equation;FN = FG momentum drag = momentum thrust + pressure thrust momentum drug =  QUOTE

Ve + (pe po) Se -  QUOTE

Vo =  QUOTE

 (Ve Vo) + (pe po) Se = 275(683.33-200) + (64.42 1)324 = 132,915.75 + 17,632.08 = 150547.83Thrust Shaft Horsepower for the modified turbojet engine will be given by the equation; thp =  QUOTE

 =  QUOTE

 = 54,744.67Propulsive efficiency (ÆÅ ¾p) for the modified turbojet engine will be given by the equation;Èp = = = = 0.4502Thermal efficiency (ÆÅ ¾th) for the modified turbojet engine will be given by the equation;ÆÅ ¾th = In order to find we use the formulae Èp = But we know that = FTV0 Therefore; = 15,0547.83 x 200 = 301,094,400Making the subject we have; = =  QUOTE

 = 66,880,053 Input energy  QUOTE

is given by; (fuel mass flow rate) x (fuel energy density) Therefore;  QUOTE

 = 275 x 2500 = 687,500lbs/hr In to BTU = 687,50... Aircraft Electrical Systems Engine Performance Coursework - 1375 Words Aircraft Electrical Systems Engine Performance (Coursework Sample) Content: AIRCRAFT ELECTRICAL AND MECHANICAL SYSTEMS: CASE STUDY AIRCRAFT ELECTRICAL SYSTEMS ENGINE PERFORMANCE(Student Name)(Course No.)(Lecturer)(University)(City State)(Date) Task 1Name of SectionExit Duct Area(Se)Exit Pressure (pe)Exit Air Velocity (Ve)Air Mass Flow ( QUOTE

) Aircraft Velocity (V0)Compressor200100350275200Diffuser220120300275200Combustion Chamber500110250275200Turbine40025900275200Exhaust60025700275200Propelling Nozzle3246.51080275200Average64.42596.67275200The thrust equation for a turbojet engine can be derived from Newtons Second law of motion, which implies that force equals the time rate of change of momentum.F =  QUOTE

For a Turbojet Engine, the Net thrust (FN) is normally given by the difference between the Gross thrust (FG) and the Momentum drug (Vinh, 1995). This is given as;FN = FG momentum drag = momentum thrust + pressure thrust momentum drug =  QUOTE

Ve + (pe po) Se -  QUOTE

Vo =  QUOTE

 (Ve Vo) + (pe po) Se = 275(596.67 200) + (64.42 1)324 = 109084.25 + 20548.08 = 129,632.33Where; W = is weight flow rate of the air passing through the engine. Ve = jet stream velocity pe = static pressure across propelling nozzle po = atmospheric pressure (given as 1 atm)Se = propelling nozzle area Vo = aircraft speed Thrust Shaft Horsepower for the turbojet engine will be given by the equation; thp =  QUOTE

 = bhpÆÅ ¾p= = 47,139Where; T = Thrust (lb)Vo = Velocity (ft/s)bhp = Engine break horsepower550 = conversion factor from ft-lbs to horsepowerÆÅ ¾p = propeller efficiencyPropulsive efficiency (ÆÅ ¾p) for the turbojet will be given by the equation;Èp = = = = = 0.5025Where; = Propulsive power output (thrust power given as FTV0) = Mechanical power input = Flight Velocity = Exit VelocityThe solution of Èp 1; this shows that not the entire mechanical power () goes into propelling the turbojet. Some of it is left as excess kinetic energy.Thermal efficiency (ÆÅ ¾th) for the turbojet engine will be given by the equation;ÆÅ ¾th = Where; m = Mechanical power i = Input energyIn order to find we use the formulae Èp =  QUOTE

 But we know that  QUOTE

 = FTV0 Therefore;  QUOTE

 = 129,632.33 x 200 = 25,926,466 Making  QUOTE

 the subject we have;  QUOTE

 =  QUOTE

 =  QUOTE

 = 51,594,957 Input energy  QUOTE

is given by; (fuel mass flow rate) x (fuel energy density) Therefore;  QUOTE

 = 275 x 2500 = 687,500lbs/hr In to BTU = 687,500 x 18,730 = 128768750 Èth = = 0.4006Overall efficiency (È0) for the turbojet engine will be given by the equation;È0 = = = Where; = the rate of energy input needed to generate the thrust = Propulsive power output (thrust power given as FTV0)Therefore; from the definitions of thermal and propulsive efficiency, the overall efficiency can also be given as;È0 = Èth x Èp È0 = 0. 4006 x 0.5025 = 0.2013Task 2Name of SectionExit Duct AreaExit Pressure (pe)Exit Air Velocity (Ve)Air Mass Flow ( QUOTE

) Aircraft Velocity (V0)Compressor20010035055200Diffuser22012030055200Combustion Chamber50011025055200Turbine4002590055200Exhaust6002570055200Propelling Nozzle3246.5108055200Fan90030500220900The thrust produced by turbofan engine is given by the equation;FN = FG momentum drag = momentum thrust + pressure thrust momentum drug =  QUOTE

Ve + (pe po) Se -  QUOTE

Vo =  QUOTE

 (Ve Vo) + (pe po) Se = 220(500-900) + (30-1)900 = 88000 + 26100 = 114,100Where; W = is weight flow rate of the air passing through the engine. Ve = jet stream velocity pe = static pressure across propelling nozzle po = atmospheric pressure Se = propelling fan area Vo = aircraft speedThrust Shaft Horsepower for the turbofan engine will be given by the equation; thp =  QUOTE

 = bhpÆÅ ¾p= = 186,70 9Where; T = Thrust (lb)Vo = Velocity (ft/s)bhp = Engine break horsepower550 = conversion factor from ft-lbs to horsepowerÆÅ ¾p = propeller efficiencyPropulsive efficiency (ÆÅ ¾p) for the turbofan engine will be given by the equation;Èp = = = = 1.285Where; = Flight Velocity = Exit VelocityThermal efficiency (ÆÅ ¾th) for the turbofan engine will be given by the equation;ÆÅ ¾th = Where; m = Mechanical power i = Input energyIn order to find we use the formulae Èp = But we know that = FTV0 Therefore;
 = 114,100 x 900 = 102,690,000 Making  QUOTE

 the subject we have;  QUOTE

 =  QUOTE

 =  QUOTE

 = 79,914,396 Input energy  QUOTE

is given by; (fuel mass flow rate) x (fuel energy density) Therefore;  QUOTE

 = 220 x 2500 = 550,000lbs/hr In to BTU = 550,000 x 18,730 = 103,015,000  QUOTE

 Èth = HYPER13 QUOTE HYPER14 = 0.7757Overall efficiency (È0) for the turbofan engine will be given by the equation;È0 = ÃƒË †th x Èp È0 = 0.7757 x 1.285 = 0.9968Task 3Name of SectionExit Duct AreaExit Pressure (pe)Exit Air Velocity (Ve)Air Mass Flow ( QUOTE

) Aircraft Velocity (V0)Compressor200100350275200Diffuser220120300275200Combustion Chamber500110250275200Turbine400251000275200Exhaust60025700275200Propelling Nozzle3246.51500275200Average64.42683.33275200The thrust produced by a modified turbojet engine is given by the equation;FN = FG momentum drag = momentum thrust + pressure thrust momentum drug =  QUOTE

Ve + (pe po) Se -  QUOTE

Vo =  QUOTE

 (Ve Vo) + (pe po) Se = 275(683.33-200) + (64.42 1)324 = 132,915.75 + 17,632.08 = 150547.83Thrust Shaft Horsepower for the modified turbojet engine will be given by the equation; thp =  QUOTE

 =  QUOTE

 = 54,744.67Propulsive efficiency (ÆÅ ¾p) for the modified turbojet engine will be given by the equation;Èp = = = = 0.4502Thermal efficiency (ÆÅ ¾th) for the modified turbojet engine will be given by the equation;ÆÅ ¾th = In order to find we use the formulae Èp = But we know that = FTV0 Therefore; = 15,0547.83 x 200 = 301,094,400Making the subject we have; = =  QUOTE

 = 66,880,053 Input energy  QUOTE

is given by; (fuel mass flow rate) x (fuel energy density) Therefore;  QUOTE

 = 275 x 2500 = 687,500lbs/hr In to BTU = 687,50...

IT Personnel Management and Its Comparison with Traditional Human Resource Management Free Essay Example, 4500 words

The recruitment of the right person in the right job at the right time is vital to the success of a company and is a key element of what the human resource department does. The process of recruitment of IT personnel is not very different from that of non-IT personnel. There are additional skills that the IT personnel should possess. The process of recruitment can be divided into three core stages starting with the definition of requirements, then the recruitment and then the selection process. (Amit and Belcourt, 1999)It is important to define the qualities, competencies and general requirements sought from the potential employee. For an efficient selection process and to avoid future problems (including high staff turnover, lack of satisfaction and wastage of resources), it is necessary to have a preset profile of the skills and abilities of the candidate. The process of defining the requirements should start with an analysis of the job. Job analysis is the collecting, analyzing an d setting out information about a job under the headings of overall purpose, content, accountability, performance criteria, competencies, responsibilities and more. We will write a custom essay sample on IT Personnel Management and Its Comparison with Traditional Human Resource Management or any topic specifically for you Only $17.96 $11.86/page