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(a)
To express: The velocity of the wind as a
(a)
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Answer to Problem 59E
The expression of wind velocity in component form is
Explanation of Solution
Given:
The speed of wind is
Formula used:
If velocity of wind is vector v which makes angle
Calculation:
The speed of wind is
The angle made by wind velocity with positive
Wind velocity vector v is shown on coordinate axis in Figure (1).
Figure (1)
Substitute
Thus, the component form of wind velocity v is
(b)
To express: The velocity of the jet relative to air in component form.
(b)
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Answer to Problem 59E
Expression of jet velocity in component form relative to air is
Explanation of Solution
Given:
The speed of Jet is
Formula used:
If velocity of Jet is vector u which makes angle
Calculation:
The speed of Jet is
So, the angle made by Jet velocity vector with positive
Jet velocity vector is shown in Figure (2).
Figure (2)
Substitute
Thus, component form of Jet velocity u is
(c)
To find: The true velocity of Jet as a vector.
(c)
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Answer to Problem 59E
True velocity of jet as a vector is
Explanation of Solution
Given:
The speed of wind is
The speed of Jet is
Formula used:
If vector u is
Calculation:
If true velocity of jet is vector p , then vector p will be the resultant sum of wind velocity v and jet velocity u.
Figure (3) shows the vector u, vector v and vector p on coordinate axis.
Figure (3)
From section (b) jet velocity u is
Substitute
And vector p is
Therefore,
Thus true velocity of jet is
(d)
To find: True speed and direction of Jet.
(d)
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Answer to Problem 59E
True speed of jet is
Explanation of Solution
Given:
The speed of Jet relative to air is
Formula used:
If
Where,
Calculation:
From Section (c), the true velocity of jet is
Substitute
Therefore true speed of jet is
If
From section (c), true velocity vector of jet is
Thus,
Solve for
So, direction is
Therefore, the true speed of jet is
Chapter 9 Solutions
Precalculus: Mathematics for Calculus - 6th Edition
- 3.12 (B). A horizontal beam AB is 4 m long and of constant flexural rigidity. It is rigidly built-in at the left-hand end A and simply supported on a non-yielding support at the right-hand end B. The beam carries Uniformly distributed vertical loading of 18 kN/m over its whole length, together with a vertical downward load of 10KN at 2.5 m from the end A. Sketch the S.F. and B.M. diagrams for the beam, indicating all main values. Cl. Struct. E.] CS.F. 45,10,376 KN, B.M. 186, +36.15 kNm.7arrow_forwardQize f(x) = x + 2x2 - 2 x² + 4x²² - Solve the equation using Newton Raphsonarrow_forward-b±√√b2-4ac 2a @4x²-12x+9=0 27 de febrero de 2025 -b±√√b2-4ac 2a ⑥2x²-4x-1=0 a = 4 b=-12 c=9 a = 2 b = 9 c = \ x=-42±√(2-4 (4) (9) 2(4)) X = (12) ±√44)-(360) 2(108) x = ±√ X = =±√√²-4(2) (1) 2() X = ±√ + X = X = + X₁ = = X₁ = X₁ = + X₁ = = =arrow_forward
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- 7.10 (B/C). A circular flat plate of diameter 305 mm and thickness 6.35 mm is clamped at the edges and subjected to a Uniform lateral pressure of 345 kN/m². Evaluate: (a) the central deflection, (b) the position and magnitude of the maximum radial stress. C6.1 x 10 m; 149.2 MN/m².] 100 200arrow_forward3.15 (B). A beam ABCD is simply supported at B and C with ABCD=2m; BC 4 m. It carries a point load of 60 KN at the free end A, a Uniformly distributed load of 60 KN/m between B and C and an anticlockwise moment of 80 KN m in the plane of the beam applied at the free end D. Sketch and dimension the S.F. and B.M. diagrams, and determine the position and magnitude of the maximum bending moment. CEL.E.] CS.F. 60, 170, 70KN, B.M. 120, +120.1, +80 kNm, 120.1 kNm at 2.83 m to right of 8.7arrow_forward7.1 (A/B). A Uniform I-section beam has flanges 150 mm wide by 8 mm thick and a web 180 mm wide and 8 mm thick. At a certain section there is a shearing force of 120 KN. Draw a diagram to illustrate the distribution of shear stress across the section as a result of bending. What is the maximum shear stress? [86.7 MN/m².arrow_forward
- 1. Let Ả = −2x + 3y+42, B = - - 7x +lý +22, and C = −1x + 2y + 42. Find (a) Ả X B (b) ẢX B°C c) →→ Ả B X C d) ẢB°C e) ẢX B XC.arrow_forward3.13 (B). A beam ABC, 6 m long, is simply-supported at the left-hand end A and at B I'm from the right-hand end C. The beam is of weight 100 N/metre run. (a) Determine the reactions at A and B. (b) Construct to scales of 20 mm = 1 m and 20 mm = 100 N, the shearing-force diagram for the beam, indicating thereon the principal values. (c) Determine the magnitude and position of the maximum bending moment. (You may, if you so wish, deduce the answers from the shearing force diagram without constructing a full or partial bending-moment diagram.) [C.G.] C240 N, 360 N, 288 Nm, 2.4 m from A.]arrow_forward5. Using parentheses make sense of the expression V · VXVV · Å where Ả = Ã(x, y, z). Is the result a vector or a scaler?arrow_forward
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