The, Antigone, And The Island By Athol Fugard - 1423 Words

Try thinking about every time you have been bullied or feel segregated from a group of people. There are countless amounts of times where we can recall a time where we feel like the odd person out or the last person picked to play kickball. â€Å"Oh, they have John! We are definitely going to win now!† are never words you want to hear about you ever. Our natural instincts as humans is bottle up all of our negative energy and attempt to forget about what had just transpired and move forward. For some people, this may be very difficult due to the fact that their life depends on it. Apartheid in South Africa segregated races in order to purify their country. It can be easily seen that most of these blacks would have been very unhappy with the government they are apart of. The negative energy doesn’t always get bottled up in this case and sometimes it leads to revolt, such as in Sophocles’, Antigone, and in The Island by Athol Fugard. Unfortunately, many people get k illed when this such event occurs. Since the entire country of South Africa is under racial prejudice, similar to Creon’s rule in Antigone, the characters in both The Island and Antigone feel the obligation to protest authority and change the course of their lives in similar methods. It is first very important to understand deep history of Apartheid to actually understand the story of The Island and the messages it sends. The beginning of Apartheid marked a big turning point in South African history. In the beginning,Show MoreRelatedThe Island by Athol Fugard2088 Words   |  9 PagesThe Island (1973) Athol Fugard A Quick Rundown of The Island - The Island is a Fugard play that resorts to the Classics to protest Apartheid. - It takes place in four scenes, opening with a lengthy mimed sequence in which John and Winston, two cell mates in prison on Robben Island, carry out one of the totally pointless and exhausting tasks designed by warders to break the spirit of political prisoners. - Winston has been sentenced to prison for life because he burned his passbook in front

Organisational Behaviour - Movie Review - 4166 Words

ORGANISATIONAL BEHAVIOUR MOVIE REVIEW ON GLADIATOR GMBA January 2008 Avinash Anand â€Å"We mortals are but Shadows and Dust Maximus†¦ Shadows and Dust!† - Proximo Summary The movie, set in 180 A.D. traces the journey of a man who goes from being a trusted army General to the Emperor of Rome to a Slave to a Gladiator who eventually defies the Empire to exact his revenge and ensure that Rome gets converted back into a Republic. The movie highlights various aspects of inter personal relationships, group dynamics, leadership qualities and personal qualities such as courage, determination, self belief, love, jealousy, ambition and most of all Power. Character Analysis Maximus (Played by Russell Crowe) The central character of the†¦show more content†¦Among managers, Type D practices constitute an ideal state from the standpoint of organizational effectiveness. Maximus is a great leader who likes honesty and trust with all members of his team. In order to build this trust and loyalty, he demonstrates his abilities on the battlefield and earns the respect and trust of his team members. Once this relationship is established, and the members are comfortable with Maximus, the leader, a two way communication process gets established wherein there is feedback as well as disclosure and this is seen especially in Maximus’s interaction with Juba. Marcus Aurelius (Played by Richard Harris) Marcus Aurelius – a great Roman Emperor with the vision of a peaceful and just empire. A philosopher – Marcus wants the world to look up to Rome as its light. He has spent all his time as Cesar to make sure that his vision of Rome is realised. Even though he holds the position of Cesar, he strongly believes in the Republic system of empire where highest powers are vested with the Senate. He puts this belief over the interests of his son who is aiming to become the next ruler of Rome. This shows the mark of a selfless leader and a visionary. He wants to appoint a morally upright man as his successor who will eventually hand over power to the senate and does this by chosing Maximus because of his integrity and capabilities. This decision ofShow MoreRelatedPerformance and Reward Issues for Mcdonalds4049 Words   |  17 PagesCONTENTS 1.0 Introduction†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦..†¦Ã¢â‚¬ ¦.pg.3 2.0 Organisational Analysis and Issues Identified†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦.pg.3 3.0 Recommendations†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦.pg.5 4.0 Action Planning†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦...pg.5 4.1 Action Planning for owner-operators, for management†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦..†¦pg.6 4.2 Action Planning for staff†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦.†¦Ã¢â‚¬ ¦.pg.7 5.0 Informal Feedback†¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦Ã¢â‚¬ ¦..†¦..pg.8 5.1 How Informal feedbackRead MoreHuman Resource Management Notes Essay example3968 Words   |  16 Pagesï » ¿MGMT 2718 Human Resource Management Notes Introduction People are our most valued resource ‘New’ emphasis on achieving organisational success through management of people HRM as the ‘organisation’s conscience’ – where workers can expect to be treated with fairness HR ‘Process’ – recruitment, selection, training and development, performance management, reward and motivation, redundancy ‘Hard’ – ‘military’ model – management as commander – dictates strategy, then HRM follows – quantitativeRead MoreThe Film Friends With Benefits as a Case Study To Explore Workplace Behavior2966 Words   |  12 Pagesapply theory appropriately. 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Flow Past Aerofoil Free Essays

ME2135E Lab Report Flow Past an Aerofoil by LIN SHAODUN Lab Group Date A0066078X 2B 10th Feb 2011 TABLE OF CONTENTS EXPERIMENTAL DATA – TABLE 1, 2, 3 2 GRAPH – ? 4 GRAPH – ? 5 GRAPH – 6 SAMPLE CALCULATION 7 DISCUSSION 8 1 EXPERIMENTAL DATA Table 1: Coordinate of Pressure Tapping Tapping No. 1 2 3 4 5 6 7 8 9 10 11 Note: Table 2: Pressure Readings Manometer inclination: Pressure Readings Pitot Pressure Static Pressure Atmospheric Pressure Atmospheric Temperature Stall angle: At the end of the experiment 474 mm 497 mm 500 mm 29 °C (mm) 0. 0 2. We will write a custom essay sample on Flow Past Aerofoil or any similar topic only for you Order Now 5 5. 0 10 20 30 40 50 60 70 80 (mm) 0. 000 3. 268 4. 443 5. 853 7. 172 7. 502 7. 254 6. 617 5. 04 4. 580 3. 279 0 0. 025 0. 049 0. 098 0. 197 0. 295 0. 394 0. 492 0. 591 0. 689 0. 787 0 0. 032 0. 044 0. 058 0. 071 0. 074 0. 071 0. 065 0. 056 0. 045 0. 032 At the beginning of the experiment 474 mm 497 mm 500 mm 29 °C 2 Manometer Readings at various Tapping 1 2 3 4 5 6 7 8 9 10 11 478 489 494 501 505 506 506 505 502 501 500 496 478 484 492 498 500 502 502 500 499 499 495 475 478 486 494 497 499 500 498 498 498 493 476 475 480 488 493 495 498 496 496 498 486 540 532 528 522 518 516 514 507 503 502 509 562 550 546 526 522 518 514 508 504 502 495 523 520 520 518 517 516 516 515 515 515 498 516 514 515 516 515 514 514 512 513 514 Table 3: Pressure Coefficients ( ) Free Stream Velocity v v v ( ) Reynolds Number 3 Coefficients at various Tapping 1 2 3 4 5 6 7 8 9 10 11 -0. 956 -0. 478 -0. 261 0. 043 0. 217 0. 261 0. 261 0. 217 0. 087 0. 043 0. 000 -0. 174 -0. 956 -0. 696 -0. 348 -0. 087 0. 000 0. 087 0. 087 0. 000 -0. 043 -0. 043 0. 783 -1. 087 -0. 956 -0. 609 -0. 261 -0. 130 -0. 043 0. 000 -0. 087 -0. 087 -0. 087 2. 174 -1. 043 -1. 087 -0. 869 -0. 522 -0. 304 -0. 217 -0. 087 -0. 174 -0. 174 -0. 087 -0. 609 1. 739 1. 391 1. 217 0. 956 0. 783 0. 696 0. 609 0. 304 0. 130 0. 087 0. 391 2. 695 2. 74 2. 000 1. 130 0. 956 0. 783 0. 609 0. 348 0. 174 0. 087 -0. 217 1. 000 0. 869 0. 869 0. 783 0. 739 0. 696 0. 696 0. 652 0. 652 0. 652 -0. 087 0. 696 0. 609 0. 652 0. 696 0. 652 0. 609 0. 609 0. 522 0. 565 0. 609 GRAPH ? 3. 0 2. 5 2. 0 1. 5 CPL , CPU against X/C @ 4 ° Cpl 3. 0 2. 5 CPL , CPU against X/C @ 8 ° Cpl Cpu 2. 0 1. 5 Cpu CPL ,CPU CPL ,CPU 1. 0 0. 5 0. 0 -0. 5 -1. 0 -1. 5 0. 0 0. 1 0. 2 0. 3 0. 4 0. 5 0. 6 0 . 7 0. 8 0. 9 1. 0 1. 0 0. 5 0. 0 -0. 5 X/C -1. 0 -1. 5 0. 0 0. 1 0. 2 0. 3 0. 4 0. 5 0. 6 0. 7 0. 8 X/C 0. 9 1. 0 Area = 0. 437 Area = 0. 813 4 3. 2. 5 2. 0 1. 5 CPL , CPU against X/C @ 12 ° 3. 0 2. 5 CPL , CPU against X/C @ 16 ° Cpl Cpu 2. 0 1. 5 Cpl Cpu CPL ,CPU CPL ,CPU X/C 0. 0 0. 1 0. 2 0. 3 0. 4 0. 5 0. 6 0. 7 0. 8 0. 9 1. 0 1. 0 0. 5 0. 0 -0. 5 -1. 0 -1. 5 1. 0 0. 5 0. 0 -0. 5 -1. 0 -1. 5 0. 0 0. 1 0. 2 0. 3 0. 4 0. 5 0. 6 0. 7 0. 8 X/C 0. 9 1. 0 Area = 0. 858 GRAPH ? Area = 0. 729 3. 0 2. 5 2. 0 1. 5 CPF , CPR against Y/C @ 4 ° Cpf Cpr 3. 0 2. 5 2. 0 1. 5 CPF , CPR against Y/C @ 8 ° Cpf Cpr CPF ,CPR 1. 0 0. 5 0. 0 -0. 5 -1. 0 CPU ,CPR Y/C 1. 0 0. 5 0. 0 -0. 5 -1. 0 Y/C -1. 5 -0. 10 -0. 08 -0. 06 -0. 4 -0. 02 0. 00 0. 02 0. 04 0. 06 0. 08 0. 10 -1. 5 -0. 10 -0. 08 -0. 06 -0. 04 -0. 02 0. 00 0. 02 0. 04 0. 06 0. 08 0. 10 Area = 0. 032 Area = 0. 079 5 3. 0 2. 5 2. 0 CPF , CPR against Y/C @ 12 ° Cpf Cpr 3. 0 2. 5 2. 0 1. 5 CPF , CPR against Y/C @ 16 ° Cpf Cpr 1. 5 C PL ,CPU CPL ,CPU Y/C 1. 0 0. 5 0. 0 1. 0 0. 5 0. 0 -0. 5 -1. 0 -0. 5 -1. 0 Y/C -1. 5 -0. 10 -0. 08 -0. 06 -0. 04 -0. 02 0. 00 0. 02 0. 04 0. 06 0. 08 0. 10 -1. 5 -0. 10 -0. 08 -0. 06 -0. 04 -0. 02 0. 00 0. 02 0. 04 0. 06 0. 08 0. 10 Area = -0. 038 GRAPH Area = -0. 053 0. 437 0. 813 0. 858 0. 729 0. 32 0. 079 -0. 038 -0. 053 0. 434 0. 794 0. 847 0. 715 0. 062 0. 191 0. 141 0. 150 0. 439 0. 877 1. 316 1. 755 1. 8 1. 6 1. 4 1. 2 Cl Cd CL , CD against ? CL,CD, 2 1. 0 0. 8 0. 6 0. 4 0. 2 0. 0 2*Pi*a -0. 2 0. 0 2. 0 4. 0 6. 0 8. 0 ? 10. 0 12. 0 14. 0 16. 0 6 SAMPLE CALCULATION The sample calculation is based on Tapping 2 Table 1: Coordinate of Pressure Tapping Table 3: Pressure Coefficients 1. Air Density at 29 °C ( ) ( ) 2. Free Stream Velocity v v v ( ) 3. Reynolds Number 4. Pressure Coefficient ( ) ( ) ( ) ( ) 5. Lift and Drag Coefficient 7 DISCUSSION 1. Plot CL and CD against Please refer to Page 6. on the same graph. 2. Compare the experimentally measured CL with the Thin Aerofoil Theory prediction of . Discuss the similarity and discrepancy observed. The graph shows at small attack angle (4 ° and 8 °), the measured Lift coefficient is quite close to theoretical predicted value , this is because at small attack angle, air stream flows along the aerofoil surface smoothly without flow separation, which fulfills the basic assumption of Thin Aerofoil Theory, hence the experimental result matches with theoretical value well. When further increase attack angle, the streamline become highly curved, until at certain angle the streamline is no longer attached to the aerofoil surface and flow separation is occurred, massive turbulence wake appears on aerofoil upper surface, which greatly reduce the lift. At this moment aerofoil is actually â€Å"blocking† the air flow, hence the Lift coefficient is significantly reduced after reach Stall angle, and can no long follow the theoretical predicted value . 3. What would you expect the lift and drag force to be when At , since the 0015 aerofoil is symmetrical, the pressure on upper and lower surface of aerofoil is the same, hence it will not produce any lift force. The of 0015 aerofoil is 0. 0147 at (when Re=80000), so there is small drag force even at 8 4. Does the why. which you have obtained gives the total drag on the aerofoil? Explain Total Drag of aerofoil is contributed by Parasite Drag and Induced Drag, the Parasite Drag is related to , while Induce drag is a byproduct of lift. Induce drag is a drag force occurs when aerofoil redirects the airflow coming at it. Refer to below diagram, the lift force is normal to chord of aerofoil, when decompose the lift force to horizontal and vertical component, the horizontal component , which is in the same direction of drag. 5. Explain from the pressure distribution why there is a lift force. Using as example, the pressure distribution diagram shows the lower surface of aerofoil has lesser pressure drop ? igher pressure, while upper surface of aerofoil has much higher pressure drop, result in lower pressure. The integration of pressure drop along the aerofoil is the area under the curve, which represents force in a unit length of aerofoil, compare the area enclosed for upper and lower surface, we can see the there is a resultant lift force produced. 3. 0 2. 5 2. 0 1. 5 CPL , CPU against X/C @ 8 ° Cpl Cpu CPL ,CPU 1. 0 0. 5 0. 0 -0. 5 -1. 0 -1. 5 0. 0 0. 1 0. 2 0. 3 0. 0. 5 0. 6 0. 7 0. 8 0. 9 1. 0 X/C 9 6. Comment on the pressure distribution on the aerofoil when stall is reached. Using as example, when stall angle is reached, the pressure drop of upper surface become insignificant due to massive turbulent wake, hence the lift force is greatly reduce and stall happens. 3. 0 2. 5 2. 0 1. 5 CPL , CPU against X/C @ 16 ° Cpl Cpu CPL ,CPU 1. 0 0. 5 0. 0 -0. 5 -1. 0 -1. 5 0. 0 0. 1 0. 2 0. 3 0. 4 0. 5 0. 6 0. 7 0. 8 X/C 0. 9 1. 0 10 How to cite Flow Past Aerofoil, Papers

Treasury and Risk Management Samples †MyAssignmenthelp.com

Question: Discuss about the Treasury and Risk Management. Answer: Determining the fairly, over and under priced future contracts: Risk free rate 0.80% Cost per ounce $ 3.00 Delivery data (months) (A) Future price per ounce (B) Current spot price (C) Discounting (D=e-0.80%*A) Exp spot price (E=(B*D)(3*A) Difference E-C Indication 1 $ 1,293.48 $ 1,280.00 0.99 $ 1,280.17 $ 0.17 Fairly priced 2 $ 1,310.66 $ 1,280.00 0.98 $ 1,283.86 $ 3.86 Overpriced 3 $ 1,318.77 $ 1,280.00 0.98 $ 1,278.50 $ (1.50) Underpriced 6 $ 1,358.99 $ 1,280.00 0.95 $ 1,277.30 $ (2.70) Underpriced From the evaluation of above calculation only the first contract is identified as fairly priced, while the rest contracts are either underpriced or overpriced. This mainly indicates that the overall futures contract needs to be drafted much better for reducing the arbitrage opportunity (Chance and Brooks 2015). Identifying the arbitrage opportunity by inspecting each contract against the spot gold price: Risk free rate 0.80% Cost per ounce $ 3.00 Delivery data (months) (A) Future price per ounce (B) Current spot price (C) Discounting (D=e0.80%*A) Exp spot price (E=(C*D)(3*A) Difference E-B 1 $ 1,293.48 $ 1,280.00 1.01 $ 1,293.28 $ (0.20) 2 $ 1,310.66 $ 1,280.00 1.02 $ 1,306.64 $ (4.02) 3 $ 1,318.77 $ 1,280.00 1.02 $ 1,320.09 $ 1.32 6 $ 1,358.99 $ 1,280.00 1.05 $ 1,360.94 $ 1.95 The overall gold futures contract could eventual help in identifying the profit that could be generated from the investment. There is relevant arbitrage opportunity that could be identified from the gold prices from today, which is seen in the above table. There is relevant arbitrage opportunity, which could be used by the individual investors to generate riskless trade from investment. From months 3 and 6 overall future price is less than spot future price, which directly allows the investors to gain extra income from their investment in futures. Bodie (2013) mentioned that increasing future price could eventually allow the investor to generate higher revenue from investment. Describing the arbitrage opportunity by combining two futures: The combination of Futures for 3 month and futures for 6 month eventually helps in identifying the Arbitrage opportunity. From the evaluation of table 1 and table 2, significant information can be gathered regarding future value and spot value of the gold contact. Difference between future contract and the expected spot price in future is relatively positive for 3 months future and negative for 2 months future.This only indicates that using 3 months future relevant arbitrage opportunity could be used by the investor for an additional benefit of $1.32. Therefore, buying future contract of 3 months and selling the spot 3 months future could eventually help in gaining and overall profit of $1.32 per gold future contract. This measure could eventually help reducing the risk from trades. However, Lam (2014) argued that assumptions in investments are subject to market risk, which could change with the changing external environment. There is an alternative strategy, where 2 months old furni ture could be sold in the current levels, whereas future spot price in two months could be bought. This could eventually help in getting a profit of $4.02 from the investments conducted in 2 months future contract. References Bodie, Z., 2013.Investments. McGraw-Hill. Chance, D.M. and Brooks, R., 2015.Introduction to derivatives and risk management. Cengage Learning. Lam, J., 2014.Enterprise risk management: from incentives to controls. John Wiley Sons.