EAS 4101 - Aerodynamics – Spring 2010
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4/19/10, Final Exam Review
Announcements:
1.
The final exam is Thursday, 4/29/09 from 5:30 pm– 7:30 pm in TBD (exam group 29e).
2.
The exam will cover up all material presented in the class.
It will be more comprehensive in
nature than the second exam, but will somewhat emphasize material covered after finite wing
theory.
Exam Format:
1.
Bring a pen
.
DO NOT bring your notes, textbook, calculator, crib sheet, etc.
2.
I anticipate that we will have several problems and several short-answer questions (T/F,
multiple choice, etc.) with the points per problem/question clearly labeled.
This may change.
3.
Below are topics that you are responsible for, the majority has been covered in class, but
some material just covered via reading assignments will also be included on the exam.
Exam Topics:
1.
“Section 0, Introduction to Flight”: ALL
Definitions/concepts:
Anatomy of an airplane, forces in flight, factors affecting lift and drag
2.
Chapter 1: Sections
ALL
Definitions/concepts:
Aerodynamic forces, moments, coefficients, center of pressure, aerodynamic
pressure, pi-theorem, flow similarity (geometric, kinematic, dynamic), stalling speed, hydrostatics,
manometers, types of flow (physical understanding), pressure and shear stress distributions and their
relationships to aerodynamic forces and moments, dimensionless force and moment coefficients
Text Examples:
1.1-1.5, design box (pg 45)
HW:
5 (problems 1-5)
3.
Chapter 2: Sections
2.1-2.16, 2-18
Definitions/concepts:
solid, fluid (liquid vs. gas), basic vector calculus, basic equations, system,
field, Eulerian, Lagrangian, kinematic decomposition, continuum assumption, steadiness,
unsteadiness, system, field, flow visualization: streaklines, pathlines, streamline computation,
Newton’s second law, body forces, surface forces, and pressure, viscosity, Newtonian flow,
deformation rate, no-slip condition, body forces, surface forces, pressure,
CV analysis
: system, open CV, extensive/intensive properties, inertial CV, RTT, continuity
equation, mass flow rate, volume flow rate, average velocity, momentum equation, etc.
Differential analysis: