Problem 5. Air flows at a velocity of U = 20 m/s over a flat bottomed, two-dimensional object with a chordlength of c = 1.0 m and wing span of 6 = 5.0 m as shown. The shape of the object, y = f(x), and thepressure distribution. p = g(x), measured in a wind tunnel with air at STP along the top surface are given in thetable. (a) Calculate and plot the pressure coefficient, C, versus * for the top of the object. (b) Calculate the liftcoefficient, Cr, using the calculated Co. (c) Calculate the lift for the object for these conditions and at a standardcruising altitude of 10 km (assuming constant C₂).UPooI** = x/cy* = y/cp-Pro (Pa)0.0000.00002450.0250.0372140.0500.0530-1270.0750.0648-1520.1000.0743-1510.2000.0992-1540.3000.1114-1660.4000.1149-1740.5000.1045-1740.6000.0911-1050.7000.0646-330.8000.0362260.9000.0126651.0000.000085

Step 1:FormulaeThe coefficient of pressure can be calculated using,…

Answered: Problem 5. Air flows at a velocity of U…

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

help
9. The thin ( 3 mm ) thick plastic panel shown in the figure is lowered from a ship to a construction site on the осean Поог. The plastic panel weighs ( 200 N) in air and is lowered at a rate of ( 2 m/s ). Assuming the ship Cble panel remains vertically oriented, calculate the tension force in the cable. Take ( p = 1000 10 m/s ), and use; kg/m', v 1.31 water Plustic Punel Cplam = 1.328/ Re, Cpturb = 0.072/Re 1/5
Problem 6.2 The gap between a moving plate of height H and a stationary wall is filled with an incompressible liquid with density pliq. The plate is pushed to the right at a constant speed Vplate. At the bottom sliding joint, there is a seal to prevent leakage. The gap width x and the liquid height y are continuously changing with time. The length dimension L into the page is constant. Side View: H V plate seal X Stationary wall (a) Determine rate of change of the liquid width with time, (d x/d t) in terms of the given variables (i.e., Vplate). (b) Assume the moving plate height H is tall enough that the liquid does not spill over. Determine the rising rate of the liquid top surface (d y/d t) in terms of the given variables. (c) Assume the moving plate height H is too short and the liquid spills over as the plate keeps moving. Determine the mass flow rate of the spillage in terms of the given variables.
A B-2A is flying at 42,500 ft in standard day conditions at 420 KTAS. The mean chord length is 39.6ft.A) Find the overall or total Reynolds number for the aircraft.
The purpose of this problem is to give you a feel for the magnitude ofReynolds number appropriate to real airplanes in actual flight. a. Consider the DC-3 shown in (1.1). The wing root chord length(distance from the front to the back of the wing where the wing joinsthe fuselage) is 14.25 ft. Consider the DC-3 flying at 200 miles perhour at sea level. Calculate the Reynolds number for the flow over thewing root chord. (This is an important number, because as we will seelater, it governs the skin-friction drag over that portion of the wing.)b. Consider the F-22 shown in (1.5), and also gracing the cover ofthis book. The chord length where the wing joins the center body is21.5 ft. Consider the airplane making a high-speed pass at a velocityof 1320 ft/s at sea level (Mach 1.2). Calculate the Reynolds number atthe wing root.
If a body with a linear dimension of 1 ft is moving in a fluid with velocity q, find the Froude number and the Reynolds number for the follow- ing cases: (a) when the fluid is air and has 4 100 ft/sec; (b) when the 1 fluid is water and has q - 5 ft/sec.
9. The thin ( 3 mm ) thick plastic panel shown in the figure is lowered from a ship to a construction site on the ocean floor. The plastic panel weighs ( 200 N) in air and is lowered at a rate of ( 2 m/s ). Assuming the ship Cble panel remains vertically oriented, calculate ing the tension force in the cable. Take ( p = 1000 * 10* m²/s ), and use; water Plastic funel kg/m', v = 1.31 m Colam = 1.328 / Re Cpturb = 0.072 / Re
A 2-1/2 inch fire hose discharges water through a nozzle having a jet diameter of 1 inch. Thelost head in the nozzle is 5.76 percent of the velocity head in the jet. If the gage pressure atbase of nozzle is (a) 86 lb per sq in.: (b) 167 lb per sq in.: (1.1) compute the discharge ingallons per minute: (1.2) what is the maximum horizontal range to which the stream can bethrown, neglecting air resistance?
Problem 1: Write the boundary conditions for the following flows: a) Flow between parallel plates (Fig. 1) without a pressure gradient. The upper plate is moving with velocity V. y = +h y = -h Fixed Fig. 1 V u(y)
Note:- • Do not provide handwritten solution. Maintain accuracy and quality in your answer. Take care of plagiarism. • Answer completely. • You will get up vote for sure.
This is for engineering fluid mechanics
Solve the following problem. View image. Give complete and detailed solutions. Given: Asked: Solution: Please write legibly.

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS