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Standards |
Posted:
FTP 106
– Aerodynamics
Provides a study of basic
aerodynamics and its relationship to the functional design of aircraft. Topics include:
incompressible flow airfoil theory, wing theory, calculation of drag and stall
speed, basic aircraft performance criteria, aircraft configuration changes,
high and low speed conditions, special flight conditions, and introduction to
compressible flow.
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Competency Areas: |
Hours: |
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Incompressible
Flow Airfoil Theory |
Class |
3 |
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Wing
Theory |
D. Lab |
0 |
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Calculation
of Drag and Stall Speed |
P.
Lab/O.B.I. |
0 |
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Basic
Aircraft Performance Criteria |
Credit |
3 |
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Aircraft
Configuration Changes |
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High and
Low Speed Conditions |
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Special
Flight Conditions |
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Introduction
to Compressible Flow |
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Prerequisite: Program admission |
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Corequisite: |
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Course Guide |
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Competency |
After completing this section,
the student will: |
Hours |
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Class |
D. Lab
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P. Lab/ O.B.I. |
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INCOMPRESSIBLE
FLOW AIRFOIL THEORY |
4 |
0
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0 |
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Lift |
Define
lift as applicable to airfoil theory. |
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Thrust |
Define
thrust as applicable to airfoil theory. |
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Drag |
Define
drag as applicable to airfoil theory. |
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Factorial
relationship |
Determine
the relationship of temperature, density, and pressure to lift, thrust, and
drag. |
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WING THEORY
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5 |
0
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0 |
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Chord |
Define
chord as applicable to wing theory. |
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Angle of
attack |
Define
angle of attack as applicable to wing theory. |
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Stall |
Define
stall as applicable to wing theory. |
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Relative
wind |
Define
relative wind as applicable to wing theory. |
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Pressure
center |
Describe
center of pressure. |
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Factorial
relationship |
Explain
the relationship of wing theory factors to other factors. |
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CALCULATION OF DRAG AND STALL SPEED
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3 |
0
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0 |
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Parasitic
drag |
Explain
parasitic drag. |
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Induced
drag |
Explain
induced drag. |
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Drag/speed |
Compare
the effects of drag on aircraft speed. |
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BASIC AIRCRAFT
PERFORMANCE CRITERIA
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3 |
0
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0 |
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Power |
Define
power. |
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Horsepower |
Define
horsepower. |
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Aircraft
performance |
Explain
the effects of drag and horsepower. Describe
the impact of these effects on aircraft performance. |
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AIRCRAFT CONFIGURATION CHANGES
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6 |
0
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0 |
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Types of aircraft |
State examples of tricycle gear, high
wing, monoplanes, low wing monoplanes, tailwheel
monoplanes, multi-engine aircraft, push type aircraft, and retractable gear
aircraft. |
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State
examples of rotor type aircraft, float type aircraft, canard type aircraft,
and multi-winged aircraft. |
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HIGH AND LOW SPEED
CONDITIONS
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3 |
0
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0 |
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Speed of
sound |
Explain
slow speed flight. |
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Explain
the relationship between airflow below the speed of sound, and airflow around
mach I. |
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Speed/performance |
Compare
the behavior of air on aircraft performance at speeds above and below mach I. |
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SPECIAL FLIGHT
CONDITIONS
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3 |
0
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0 |
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Density
altitude |
Describe
the effects of atmospheric density on flight. |
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Pressure
altitude |
Describe
the effects of altitude changes on flight. |
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Temperature |
Describe
the effects of temperature on pressure and density and on the behavior of
air. |
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INTRODUCTION TO
COMPRESSIBLE FLOW
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3 |
0
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0 |
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Speed of
sound mach number |
Define
speed of sound. Explain
mach number. |
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Shock
waves |
Compare
speed of sound and mach number relative to temperature in the production of
shock waves. |
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Suggested Resourc es |
Books:
Crane, D. (Ed.). (1991). Dictionary of aeronautical terms
(2nd ed.).
FAA. (Annual).
FAR/AIM 95.
Gladney, D. (1989). Private
pilot groundschool guide.
Guilkey,
J. E., & Snyder, C. (1993). Simplifying the FAR/AIM: An
essential guide for the private pilot.
Hurt, H. H. (1992). Aerodynamics for naval aviators.
Smith,
H. (1992). The illustrated guide to
aerodynamics.
Audiovisuals:
Jeppesen,
S.
(1992). Advanced aerodynamics: Angle
of attack [VHS, 27:30].
Jeppesen,
S.
(1992). Basic aerodynamics [VHS,
28:02].
Jeppesen,
S.
(1995). Aircraft systems and
performance [Transparencies, set of 28].
Jeppesen,
S.
(1995). Airplane and components set
[Transparencies, set of 18].
Jeppesen,
S.
(1995). Principles of flight
[Transparencies, set of 26].
Jeppesen,
S.
(1995). Weight and balance kit
[Transparencies, set of 6].
Training Aids:
Jeppesen,
S.
(Year). Model airplane kit [Wingspan,
14"].