Concept explainers
Derivation of wind turbine formula A derivation of toe function R in Exercise 69, based on three equations from physics, is outlined here. Consider again the figure given in Exercise 69, where v_1 equals the upstream velocity of the wind just before the wind stream encounters the wind turbine, and equals the downstream velocity of the wind just after the wind stream passes through the area swept out by the turbine blades. An equation for the power extracted by the rotor blades, based on conservation of momentum, is
a. Another expression for the power extracted by the rotor blades, based or conservation of energy is
b. Show that
c. If the wind were to pass through the same area A without being disturbed by rotor blades, the amount of available power would be
Want to see the full answer?
Check out a sample textbook solutionChapter 4 Solutions
Calculus: Early Transcendentals and MyLab Math with Pearson eText -- Title-Specific Access Card Package (3rd Edition) (Briggs, Cochran, Gillett & Schulz, Calculus Series)
Additional Math Textbook Solutions
Basic Business Statistics, Student Value Edition
University Calculus: Early Transcendentals (4th Edition)
Using and Understanding Mathematics: A Quantitative Reasoning Approach (6th Edition)
A First Course in Probability (10th Edition)
Precalculus
Calculus for Business, Economics, Life Sciences, and Social Sciences (14th Edition)
- Example: If ƒ (x + 2π) = ƒ (x), find the Fourier expansion f(x) = eax in the interval [−π,π]arrow_forwardExample: If ƒ (x + 2π) = ƒ (x), find the Fourier expansion f(x) = eax in the interval [−π,π]arrow_forwardPlease can you give detailed steps on how the solutions change from complex form to real form. Thanks.arrow_forward
- Examples: Solve the following differential equation using Laplace transform (e) ty"-ty+y=0 with y(0) = 0, and y'(0) = 1arrow_forwardExamples: Solve the following differential equation using Laplace transform (a) y" +2y+y=t with y(0) = 0, and y'(0) = 1arrow_forwardπ 25. If lies in the interval <0 and Sinh x = tan 0. Show that: 2 Cosh x= Sec 0, tanh x =Sin 0, Coth x = Csc 0, Csch x = Cot 0, and Sech x Cos 0.arrow_forward
- Algebra & Trigonometry with Analytic GeometryAlgebraISBN:9781133382119Author:SwokowskiPublisher:Cengage