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carlos harvey

carlos h.

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Th?i gian còn l?i 0:04:00 If the method of Lagrange multipliers is used to find the maximum value of \( 4 x y \) subject to the constraint \( x+2 y=40 \), work out the value of the Lagrange multiplier \( \lambda \). a. 30 b. 40 c. 50 d. 20 Clear my choice Làm xóng ...

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How did (and do) many Native American societies understand ancestry and descent to work? Quatrilineal- status and responsibilities of parenthood often passed through uncles to nephews and nieces Biliniel- where family identity and lineage can be traced equally through a female (mother's) and male (father's) line. Matrilineally-family identity and clan membership pass through the mother Patrilineally- inheritance and family identity pass through the father

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The largest group of animal-like protists are the O sporozoans. O flagellates. O ciliates. O amoeboids.

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An economist makes the following statement: "There is a principal-agent problem with respect to the relationship between the president and the Fed. But that's a good thing - it's how we can avoid a political business cycle." In general, what do economists mean by a "principal-agent problem"? By a "principal-agent problem," economists mean: A. When everyone in the organization focuses on profit without considering potential externalities. B. When there is no individual in charge of making decisions, since everyone is treated equally in the organization. C. When a person with the final say in all decisions is not employed by the organization that those decisions impact. D. When the goals and priorities of those in charge do not match the goals and priorities of the people they oversee.

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Answer: The volume of the solid generated when R is rotated about the y-axis is 72Ï€ cubic units.

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[ Select] W gases deviate somewhat from predicted behavior of ideal gases.

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It is known that Euler's theory gives n solutions (sinKL = 0 where KL = n) to the linear deferential equation that models the critical loads and deflection in columns. From these solutions arises the expression for the load P where the equilibrium is unstable, and the buckling equation is satisfied. $P_{cr} = \frac{n^2 \pi^2 EI}{L^2}$ para $n = 1, 2, 3, ...$ Since n can take the value of any real integer, there are finite critical loads for the W10 X 45 column studied above. These values of n are the deflection modes of the column and define how the column deforms. For the next columns with a length of 43 ft, modify the boundary conditions so that deflection occurs in the second mode.

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Problem 1 (20 Points): Solve the following initial value problem using the Method of Undetermined Coefficients (Superposition Annihilates); a) Evaluate the Homogeneous Solution. b) Evaluate the Particular Solution. c) Write the Total or Complete Solution and apply initial conditions to obtain the unique solution. $\frac{d^2y}{dx^2} + 4y = 4sin2x$, y(0) = 1, y'(0) = 0

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Problem Apply Kirchhoff's laws to the resistive circuit shown in Figure P8.11 to generate two sets of simultaneous linear equations. Show that the set of equations generated from applying Kirchhoff's Voltage law to the left and right loops and the set of equations generated from applying Kirchhoff's Voltage law to the left and outer loops yields the same solution for the value of the currents $i_1$, $i_2$, and $i_3$. a. To generate the first set of equations, write three equations corresponding to: 1. current law at a junction, 2. voltage law around the left loop, and 3. voltage law around the right loop. b. To generate the second set of equations, write three equations corresponding to: 1. current law at a junction, 2. voltage law around the left loop, and 3. voltage law around the outer loop. c. Use Excel to solve both sets of equations. Figure P8.11 30V $i_1$ 2? 6? $i_3$ $i_2$ 4? 12V

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3A) Explain in detail how the vortex panel/source panel method will solve the aerodynamics problems for arbitrary shape and thickness in order to calculate the aerodynamics characteristics. Students can explain through step by step procedures with the help of graphical illustration (4 Marks) 3B) By understanding the fundamental thin aerofoil theory for panel method (vortex or source panel method). Find one recent literatures on the research work that has been used these fundamental theory to solve the complex engineering problems especially in aerodynamics field.

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