ContentO 17119961O Mail - Castro Alvarez, Flavio - Ou xA learn-us-east-1-prod-fleet01-xythos.s3.amazonaws.com/5c1270dbb5a74/17119961?response-cache-control=private%2C%20max-age%3D21600&respon. ☆3. A 3-in-diameter horizontal jet of water, with velocity V= 45 ft/s, strikes abent plate, which deflects the water by 150° from its original direction.What magnitude force FR is required to hold the plate against the waterstream and what is the direction of the force? Disregard frictional losses150°3" dia. weher jetand gravitational effects. (Jet generally means an external stream which is"open to atmosphere".)R FRActivar WindowsVe a Configuración para activar Windows.13:01P Escribe aquí para buscara ) ENG14/10/2020近

Name: ContentO 17119961O Mail - Castro Alvarez, Flavio - Ou xA learn-us-eas
Uploaded: 2024-03-20T06:56:55.000Z
Channel: Bartleby
Description: ContentO 17119961O Mail - Castro Alvarez, Flavio - Ou xA learn-us-east-1-prod-fleet01-xythos.s3.amazonaws.com/5c1270dbb5a74/17119961?response-cache-control=private%2C%20max-age%3D21600&respon. ☆3. A 3-in-diameter horizontal jet of water, with veloci

Given data: Jet velocity, V=45 ftsDiameter of the jet, D=3 in=0.25 ft

Engineering

Mechanical Engineering

A 3-in-diameter horizontal jet of water, with velocity V = 45 fl/s, strikes a bent plate, which deflects the water by 150° from its original direction. What magnitude force Fg is required to hold the plate against the water stream and what is the direction of the force? Disregard frictional losses and gravitational effects. (Jet generally means an extemal stream which is "open to atmosphere".)

A 3-in-diameter horizontal jet of water, with velocity V = 45 fl/s, strikes a bent plate, which deflects the water by 150° from its original direction. What magnitude force Fg is required to hold the plate against the water stream and what is the direction of the force? Disregard frictional losses and gravitational effects. (Jet generally means an extemal stream which is "open to atmosphere".)

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

How is longitudinal stability achieved in fighter aircrafts like SEPECAT Jaguar?
Suppose we got the following data during a test of a 2- stroke engine in which gas is usedas a fuel:Diameter of the piston = 149 mmStroke length = 179 mmClearance volume = 0.88 literrpm of the engine = 302Indicated mean effective pressure = 6.0 barGas consumption = 6.0 m3/hCalorific value of the gas (fuel) = 16990 kJ/m3Make a clear sketch the geometry of this engine using the data and determine thefollowing:i. Indicated power developed by the engine in watt.ii. Air Standard Efficiencyiii. Indicated thermal efficiency of the engine.
Consider the network described in the table below.Activity ImmediatePredecessor(s)Pessimistic Probable OptimisticJ -- 15 10 8K -- 9 8 7L J 10 6 5M J 3 3 3N K,M 9 5 1O K,M 10 7 4P L,N 10 8 3a. Calculate the expected duration of each activity.b. Calculate the expected duration and variance of the critical path.c. Calculate the probability that the project will be completed in fewer than 30 time units.
pleassssse solve question 7, statics
Green Forever (see Problem S5. 12) has decided to addan automatic string feeder system with cost and revenue estimatesas shown below to the GF Deluxe model.a) What is the new revenue retrieval value for each model?b) Which model is the better environmental design alternative?
a string is attached to a mechanical vibrator, which has a frequency of 30Hx. the sttring is 3.0m long and has a linear density of .4 g/cm. the tension is varied by adding weights to teh string passing over the pully. What tension is needed to cause the string to resonate with the vibrator in four segments. assume that he points where the string meets the vibrator and the pulley are approx nodes.
ANSWER ASAP. WILL UPVOTEEEEEEEEEEEEEEEEE
Explain the concept of system reliability and its importance in the field of engineering.
Determine the blade length for a wind turbine that supplies an electrical power output of 1.95 MW and given the following parameters: Wind speed = 51 km/hr The gear, generator and electric efficiencies are 93%, 95% and 91% respectively. The power coefficient of the wind turbine is the maximum possible as given by the Lanchester-Betz limit. Assume the atmospheric air conditions are 1.01325 bar and 27 °C
URGENT.THEORY OF MACHINE A circular cutter has 4 different-sized blades, Blade A, Blade B, Blade C and Blade D, are rotating at constant velocity of 230 rad/s.The known parameters for each blade are : The weights: WA = 15 kg, WB = 25 kg, WD = 20kg The radius: RA = 300 mm, RC = 200 mm and RD = 350 mm The angle: θA = 190°; θB = 45°; θC = 90°; θD = 260° You have been asked to determine: (a) The weight of Blade C (in N) and radius of Blade B (in m) to make the whole cutter system balanced, without adding additional blade. (b) If the plane containing B and C is 0.5 m apart, determine position of planes A and D. Note: If plane A as baseline, find the length for each plane to the baseline (lb, lc, ld) (c) Sketch and label the statically balanced link of the system.
Consider a US Air Force launch of its latest GPS satellite from Cape Canaveral. Radar tracking shows the following J2000 state vector (X,Y,Z and Vx,Vy,Vz) at burnout. 26 Feb 2022 17:10:00.000 (X,Y,Z): 5210.345121 -549.481941 4300.883291 (Vx,Vy,Vz): -1.451280 7.391098 2.690198 Calculate the minimum total delta V required to maneuver this spacecraft into a circular orbit with a 12-hour period and an inclination of 61 degrees, assuming impulsive maneuvers and two-body dynamics. Please solve using equations from Howard Curtis's Orbital Mechanics for Engineering Students, 4th Edition. Or if not possible name the equations you use. If you could solve with specific angular momentum "h", earth gravitational parameter "mu", semimajor axis "a", and the target velocity for orbit "v_target". Also please use matlab syntax for solving or write the equations out clearly. Thanks!
Consider a US Air Force launch of its latest GPS satellite from Cape Canaveral. Radar tracking shows the following J2000 state vector (X,Y,Z and Vx,Vy,Vz) at burnout. 26 Feb 2022 17:10:00.000 (X,Y,Z): 5210.345121 -549.481941 4300.883291 (Vx,Vy,Vz): -1.451280 7.391098 2.690198 Calculate the minimum total delta V required to maneuver this spacecraft into a circular orbit with a 12-hour period and an inclination of 61 degrees, assuming impulsive maneuvers and two-body dynamics. Please solve using equations from Howard Curtis's Orbital Mechanics for Engineering Students, 4th Edition. Or if not possible name the equations you use. Also please use matlab syntax for solving or write the equations out clearly. Thanks!