Standards

Posted: 03/17/05

FTP 106 – Aerodynamics

Course Description:

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.

 

Competency Areas:

Hours:

Incompressible Flow Airfoil Theory

Class

3

Wing Theory

D. Lab

0

Calculation of Drag and Stall Speed

P. Lab/O.B.I.

0

Basic Aircraft Performance Criteria

Credit

3

Aircraft Configuration Changes

 

 

High and Low Speed Conditions

 

 

Special Flight Conditions

 

 

Introduction to Compressible Flow

 

 

 

 

 

Prerequisite: Program admission

Corequisite:

 

 

 

 

 

 

Course Guide

 

 

Competency

After completing this section, the student will:

Hours

Class

D. Lab

P. Lab/

O.B.I.

INCOMPRESSIBLE FLOW AIRFOIL THEORY

4

0

0

Lift

Define lift as applicable to airfoil theory.

 

 

 

Thrust

Define thrust as applicable to airfoil theory.

 

 

 

Drag

Define drag as applicable to airfoil theory.

 

 

 

Factorial relationship

Determine the relationship of temperature, density, and pressure to lift, thrust, and drag.

 

 

 

WING THEORY

5

0

0

Chord

Define chord as applicable to wing theory.

 

 

 

Angle of attack

Define angle of attack as applicable to wing theory.

 

 

 

Stall

Define stall as applicable to wing theory.

 

 

 

Relative wind

Define relative wind as applicable to wing theory.

 

 

 

Pressure center

Describe center of pressure.

 

 

 

Factorial relationship

Explain the relationship of wing theory factors to other factors.

 

 

 

CALCULATION OF DRAG AND STALL SPEED

3

0

0

Parasitic drag

Explain parasitic drag.

 

 

 

Induced drag

Explain induced drag.

 

 

 

Drag/speed

Compare the effects of drag on aircraft speed.

 

 

 

BASIC AIRCRAFT PERFORMANCE CRITERIA

3

0

0

Power

Define power.

 

 

 

Horsepower

Define horsepower.

 

 

 

Aircraft performance

Explain the effects of drag and horsepower.

Describe the impact of these effects on aircraft performance.

 

 

 

AIRCRAFT CONFIGURATION CHANGES

6

0

0

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.

 

 

 

 

State examples of rotor type aircraft, float type aircraft, canard type aircraft, and multi-winged aircraft.

 

 

 

HIGH AND LOW SPEED CONDITIONS

3

0

0

Speed of sound

Explain slow speed flight.

 

 

 

 

Explain the relationship between airflow below the speed of sound, and airflow around mach I.

 

 

 

Speed/performance

Compare the behavior of air on aircraft performance at speeds above and below mach I.

 

 

 

SPECIAL FLIGHT CONDITIONS

3

0

0

Density altitude

Describe the effects of atmospheric density on flight.

 

 

 

Pressure altitude

Describe the effects of altitude changes on flight.

 

 

 

Temperature

Describe the effects of temperature on pressure and density and on the behavior of air.

 

 

 

INTRODUCTION TO COMPRESSIBLE FLOW

3

0

0

Speed of sound mach number

Define speed of sound.

Explain mach number.

 

 

 

Shock waves

Compare speed of sound and mach number relative to temperature in the production of shock waves.

 

 

 

 

Suggested Resourc es

 

Books:

 

Crane, D. (Ed.). (1991). Dictionary of aeronautical terms (2nd ed.). Newcastle, WA: ASA, Inc.

FAA. (Annual). FAR/AIM 95. Newcastle, WA: ASA, Inc.

Gladney, D. (1989). Private pilot groundschool guide. Aurora, IL: Aviation Technical Development, Inc.

Guilkey, J. E., & Snyder, C. (1993). Simplifying the FAR/AIM: An essential guide for the private pilot. Belmont, CA: Wadsworth.

Hurt, H. H. (1992). Aerodynamics for naval aviators. Newcastle, WA: ASA, Inc.

Smith, H. (1992). The illustrated guide to aerodynamics. New York: TAB Books.

 

Audiovisuals:

 

Jeppesen, S.  (1992).  Advanced aerodynamics: Angle of attack [VHS, 27:30]. Englewood, CO: Sanderson Jeppesen.

Jeppesen, S.  (1992).  Basic aerodynamics [VHS, 28:02].  Englewood, CO: Sanderson Jeppesen.

Jeppesen, S.  (1995).  Aircraft systems and performance [Transparencies, set of 28]. Englewood, CO: Sanderson Jeppesen.

Jeppesen, S.  (1995).  Airplane and components set [Transparencies, set of 18]. Englewood, CO: Sanderson Jeppesen.

Jeppesen, S.  (1995).  Principles of flight [Transparencies, set of 26].  Englewood, CO: Sanderson Jeppesen.

Jeppesen, S.  (1995).  Weight and balance kit [Transparencies, set of 6].  Englewood, CO: Sanderson Jeppesen.

 

Training Aids:

 

Jeppesen, S.  (Year).  Model airplane kit [Wingspan, 14"].  Englewood, CO: Sanderson Jeppesen.