1- If the production engineer increases the choke size, what will happen to the Qo , Pr and Pwf? Explain that. 2- Explain the reason to calculate the value of equivalent depth for pwf from working chart. 3- Vogel's chart ( curve), describe flow from saturated oil reservoir. His empirical equation allows us to: a) Create an IPR with only a single flowing test b) Create a combined IPR (generalized Vogel's formula) if flow is above and below the bubble point c) A and b. 4- The production engineer can't use the same Pump Characteristic Curves for every ESP, explain why he can't. 5- sketch the relation between the pressure "psi" vs. radius "ft ", of reservoir and show all the parts of the relation on it. give an example.

1- If the production engineer increases the choke size, what will happen to the Qo , Pr and Pwf? Explain that. 2- Explain the reason to calculate the value of equivalent depth for pwf from working chart. 3- Vogel's chart ( curve), describe flow from saturated oil reservoir. His empirical equation allows us to: a) Create an IPR with only a single flowing test b) Create a combined IPR (generalized Vogel's formula) if flow is above and below the bubble point c) A and b. 4- The production engineer can't use the same Pump Characteristic Curves for every ESP, explain why he can't. 5- sketch the relation between the pressure "psi" vs. radius "ft ", of reservoir and show all the parts of the relation on it. give an example.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

Each time a double-acting hydraulic cylinder extends and retracts through an 8-in. stroke cycle, a large drop of oil is seen to drip from the front seal. If the cylinder rod has an O.D. of 2 in., and the oil film thickness is 0.0008 in., what is the volume of this "drop of oil" for one cycle?
Hydraulics What is the pressure 6.1m below an oil surface (sg = 0.8)?
With the given pipe lengths, sizes and connections and if all pipes have an f=0.020. 1. which of the following most nearly gives the flow in pipe 2? a. 7 cfs b. 6 cfs c. 5 cfs d. 11 cfs 2. which of the following most nearly gives the head loss between B and C? a. 60 ft b. 100 ft c. 40 ft d. 80 ft with solution pls
Hello dears,Please answer all the Question with brief explanation [ Please answer it all I know the Guidelines but it's easy ,I will Thumb up your effort ]
Choose Correct Answer .Crudes are petroleum before Drilling. Finding. Refining. ?What is the name of the space between the drill pipe and the side of borehole Shale Shaker. Annulus. Swivel. The basic production mechanism in naturally flowing wells is result of .difference Temperature Minerals Pressure 0 0 0 ?......................A crud of low viscosity contains a large amount of dissolved under Low pressure. Low temperature Considerable pressure.
Identify the function of the following types of valves (control or isolation or safety) a) Butterfly valve b) Globe Valve c) Check Valve / NRV / One-Way valve d) Knife gate valve e) Needle valve
Show complete and correct solution, thank you.
Slip of a reciprocating pump is negative, when____ A•suction pipe is short and pump is running at low speeds B•delivery pipe is long and pump is running at high speeds C•suction pipe is short and delivery pipe is long and the pump is running at low speeds D•suction pipe is long and delivery pipe is short and the pump is running at high speeds.
Given the conditions on a converging-diverging wind tunnel. At the reservoir pressure is measured to be 200,000 Pa and density is 1.4 kg/m^3. At the throat section Mach number is 1.0 and speed of sound is 390 m/s. At the exit/exhaust the Mach number is 2.5.
State whether the statement is true or false, and if it is false, correct it. (Don't explain. Don't draw. Just write the corrected statement) A. Airfoil camber is the maximum distance between the mean camber line and the chord line, measured perpendicular to the mean camber line. B. For cambered airfoil, the lift is not equal to zero at zero angle of attack. C. Critical Mach number of an airfoil is the first supersonic free stream mach number. D. Induced drag is the drag due to high angle of attack E. Propeller blades are twisted to increase its structural strength.
A) What is the apparent viscosity (Pa.s) of blood that is experiencine a shear rate of 52 s^-1? Assume the blood has a yield stress of 0.005 pascals and a value of 2 cP^1/2 for the parameter.
The friction loss in laminar flow can be calculated using ____________ A. P.K Swammee and A.K. Jain Equation B. Darcy's equation C. Hazen-Williams Equation D. Hagen-Poiseuille equation