ME 303 FALL 2000 WSU
FINAL EXAM STUDY GUIDE
BRIEF COURSE TOPIC OUTLINE
- dimensions and units
- fluid properties
- hydrostatics
- pressure variation in non-flowing fluids; e.g. reservoirs and the "standard atmosphere"
- pressure variation in stagnant fluid with constant density: equation of hydrostatics
- resultant force (magnitude and line of action) arising from pressure on submerged surfaces
- bouyancy and floatation - Archimedes' principles
- stability of floating and submerged bodies
- ideal (frictionless) flow on a streamline: Bernoulli's equation (aka Field, Euler, "s" equation); (Euler's) "n" equation
- conservation laws, rate-of-creation bookeeping, and use of control volume analysis
- conservation of MASS
- conservation of MOMENTUM (a vector!); "force checklist" ; concept of THRUST associated with a fluid jet
- conservation of ENERGY; especially "hydraulic" form (with head losses)
- dimensional analysis
- Buckingham theorem, finding "pi" groups
- frequently encounted "pi" groups - e.g. Reynolds, Froude, Weber, Mach
- dimensional homogeneity, similitude & model testing
- internal (pipe) flow
- pipe flow: laminar/turbulent flow; influence of roughness and Reynolds number; hydraulic diameter
- calculation of pipe friction losses using Darcy-Weisbach law with friction factor from Moody chart
- uniform flow in an open channel: Manning equation
- losses in components ("minor" losses); KL (loss factor) and Lequiv (equivalent length method)
- piping systems; incorporation of pump, fan, and/or turbine in flow systems; pump (fan)/turbine efficiency
- pumps: pump head vs. flow (pump curve) vs system curve; pump NPSHA, pump selection
- external flows
- boundary layer growth and skin friction drag Cf for flow over a thin flat plate; use of flat plate drag
- drag - frictional & form; terminal velocity, drag coefficent CD
- lift - airfoil, wing, lift coefficient CL, angle-of-attack... drag caused by lift (induced drag)
- principles of flight: lift=weight, drag=thrust; stability and control of flight; wing design
Tips for the ME 303 Final Exam:
problems will be comparable in difficulty to those on quizzes
comprehensive coverage of entire course - lecture, homework, and assigned text reading
read all problems and show some work on each to receive partial credit
be ready to use tables/graphs in text
identify freebody/streamline/control volume used in analysis
briefly state any assumptions/ simplifications
insert numerical values with units as final step of analysis
always check for consistency of dimensions & units!
a numerical answer is meaningless without associated units!