Collection

2013 GSW

Authors

Yucheng Liu P.E.

represents heat transferout of the system. From different cycles, we have:For power cycle Wcycle = Qin – Qout, thermal efficiency η = Wcycle/Qin (7)For refrigeration cycle Wcycle = Qout – Qin, coefficient of performance β = Qin/Wcycle (8)For heat pump cycle Wcycle = Qout – Qin, coefficient of performance γ = Qout/Wcycle (9) Proceedings of the 2013 ASEE Gulf-Southwest Annual Conference, The University of Texas at Arlington, March 21 – 23, 2013. Copyright©2013, American Society for Engineering EducationIn above equations the Wcycle, Qin, Qout can also be replaced by the rate form Wcycle , Q in , andQ out , which

Collection

2013 GSW

Authors

Amen I. Omoragbon; Gary J. Coleman; Lex Gonzalez; Brandon Watters; Bernd Chudoba

Collection

2013 GSW

Authors

S. Nasrazadani; Devon Henkis

 “unstable” equilibrium position whereas at the local minima position the ball will be at the stable equilibrium.Equation (3) is actually the heart of Green’s Theorem that is given as follows:Let C be a peicewise-smooth, simple closed curve that bounds a region R in the plane5. If P andQ have continuous partial derivatives on an open set that contains R, then cPdx + Qdy = R ( Q/ x) - ( P/ y) dA ……………………….. (5)Equation (5) represents a closed curve region that for a conservative vector field represent acircle if the integral equals zero as equation (3) indicated but if it is a non-zero for a vector fieldsuch as (F=yi –xj) it can represent a non closed circle such as a spiral shown bellow (Figure 2) Figure 2

Collection

2013 GSW

Authors

Lynn Peterson; James Epperson; Ramon Lopez; Kevin Schug; Carter Tiernan

compared to a 51% pass rate for students not in the AURAS seminar, and have a droprate of 0% compared to a drop rate of 18% for students not in the AURAS seminar.Fall 2010, Spring 2011 & Fall 2011 compositeCourse A B C Pass D F I Q W Drop TotalMath 1323* ESP 5 16 6 56% 3 8 0 0 10 21% 48Math 1323* non-ESP (1) 13 14 24 35% 10 34 0 3 48 35% 146Math 1323* non-ESP (2) 57 84 96 42% 62 108 1 8 146 27% 562Math 1426 ESP 15 14 12 80% 8 0 0 0 2 4% 51Math 1426 non-ESP (1) 17 34

Collection

2013 GSW

Authors

Nripendra N. Sarker; Mohan A. Ketkar

created to start with. The majorsettings for the project are shown in Figure 3. The selection, “Schematic”, highlighted with a red oval, indicates that this would be a schematic project. As an example of a circuit diagram, apositive-edge triggered D Flip-Flop as shown in Figure 4, would be created extracting circuitelements from the editor. This flip-flop circuit has one input, designated with name, “D” and another input, designated with name, “Clock”.  The single output is named as, “Q”.  This will besaved as a schematic (.sch) file associated with the project.These two inputs and one output are mapped to the Nexys 2 board in a “User Constraint File” (.ucf) file as shown in Figure 5. The On/Off switches and the toggle switches in the Nexys

Collection

2013 GSW

Authors

Chaudhry M. A. Arafat; Mohammad R. Hasan; Panos S. Shiakolas; Samir M. Iqbal

., Borenstein, J. T., Cuiffi, J. D., 2011, “Membrane- integrated microfluidic device for high-resolution live cell imaging”, Biomicrofluidics, Vol. 5, No. 4, pp. 046501.3. Gerlich, D., Koch, B., Dupeux, F., Peteras, J., Ellenberg, J., 2006, “Live-cell imaging reveals a stable cohesin- chromatin interaction after but not before DNA replication”, Current Biology, Vol. 16, No. 15, pp. 1571-1578.4. Chan, E. M., Daley, G. Q., Hartung, O., Huo, H., Ince, T. A., Loh, Y., Manos, P. D., Miller, J. D., Park, I., Ratanasirintrawoot, S.,  Rho, J., Schlaeger, T. M., 2009, “Live cell imaging distinguishes bona fide human iPS  cells from partially reprogrammed cells”, Nat. Biotechnol, Vol. 27, pp. 1033+.5. Isherwood, B., Timpson, P., McGhee

Collection

2013 GSW

Authors

Amit Oza; Gary Coleman; Lex Gonzalez; Bernd Chudoba; Paul Czsyz

requirement for given stall speed and Performance Landing Coleman [5] maximum trimmed lift coefficient. 2-D energy integration method (altitude and velocity), Trajectory constant q trajectory to cruise velocity, cruise climb, Appendix A maximum L/D descent. HyFAC [3] Czysz Stability and Control Trim effects Engine cowl location effect on