Foilsim 3 online

This syllabus was developed for online learning. ASCI_309_Online_Syllabus_10/08/15

ASCI 309 Aerodynamics

Online Course Syllabus

Credit Hours: 3 Delivery Method: Online (Internet / Canvas). Required Course Materials

Dole, C. E., & Lewis, J. E. (2000). Flight theory and aerodynamics (2nd ed.).

New York, NY: Wiley & Sons. ISBN: 978-0471370062

Hurt, H. H. (1965). Aerodynamics for naval aviators (Revised ed.). NAVWEPS

00-80T-80, United States Navy. Reprinted by Aviation Supplies & Academics. ISBN: 978-1560271406

Scientific Calculator A scientific calculator will be required for assignments in this course; however, instead of a physical device, electronic means such as Windows Calculator (in Scientific mode) can be utilized.

American Psychological Association. (2010). Publication manual of the

American Psychological Association (6th ed.). Washington, DC: Author.

(APA Website: http://www.apastyle.org/manual/index.aspx)

http://www.apastyle.org/manual/index.aspx
Page 2 of 9

Course Description Students are provided with an opportunity to explore incompressible flow airfoil theory and wing theory. Topics center on: calculation of stall speed, drag and basic performance criteria, configuration changes, high and low speed conditions, special flight conditions, and an introduction to compressible flow. Prerequisite: RSCH 202 Prerequisites

 MATH 112: College Mathematics for Aviation II

 PHYS 102: Explorations in Physics Strongly Recommended Knowledge Base by Topic

 Algebra

 Trigonometry

 Physics Course Goals This course is designed to provide students with the technical background necessary to understand the operating limitations and procedures of modern airplanes and to optimize pilot technique by properly defining required tasks. Master Course Outline Learning Outcomes

Upon successful course completion, students will be able to:

1. Using “SI” and British Gravitational System of measurement, solve aeronautical flight mechanic problems involving laws of motion, forces and energy.

2. Identify standard atmospheric variables and their sea level values. Compute atmospheric conditions using the universal gas laws.

3. Identify and define the relationships between indicated, calibrated, equivalent and true airspeeds and how they change with altitude and temperature.

4. Describe the effects of velocity, density, area and lift coefficient on lift. Solve stall speed problems and learn airfoil nomenclature and designations.

5. Explain wing stall patterns and factors affecting the stall. As well as explain the aerodynamic characteristics of spins and spin recovery.

6. Explain and describe the effects of flaps, slats, vortex generators and boundary layer devices on lift, drag and pitching moment coefficients.

7. Demonstrate and understand the factors affecting maximum performance events such as best range, max endurance, best glide, max angle climb and max rate of climb.

Page 3 of 9

8. Explain stability, controllability and the factors in high speed flight such as speed ranges, critical Mach number, the Force Divergent Mach number, Mach tuck, control buzz and shockwaves.

9. Demonstrate and discuss the origin and effects of induced drag and methods utilized to reduce induced drag.

10. Explain factors affecting the maneuvering envelope and solve problems involving the turn equations.

Worldwide Learning Outcomes

Upon successful course completion, students will be able to:

11. Discuss how wing planform characteristics, i.e. wing area, wing span, mean aerodynamic chord, taper ratio, aspect ratio, affect lift, drag and aircraft performance.

12. Determine maximum range, endurance speeds and rate of climb airspeeds from

plots of power, thrust and drag versus airspeed and understand wind and fuel flow effects.

13. Describe the cause and effects of compressibility and the aerodynamic design features for high-speed transonic and supersonic flight.

14. Describe aircraft stability and control, including the aircraft features that improve or degrade stability and control and the flight conditions where stability and control are critical

15. Determine the origins and effects of parasite drag and methods utilized to reduce it.

16. The student will demonstrate appropriate selection and application of a research method and statistical analysis (where required), specific to the course subject matter.

Page 4 of 9

Grading Policy All evaluated activities and deliverables carry a maximum possible score of 100. The Grade Center in Canvas automatically calculates and weights the scores according to categories that make up the final course grade (see the table below). Consequently, your final grade is based on the weighted scores, not a total score. If you have questions about the grading policy, please contact your instructor privately.

Course Grade Scale Evaluation Items & Weights

90 – 100% A Discussion 20%

80 – 89% B Exercises 30%

70 – 79% C Midterm Exam 25%

60 – 69% D Final Exam 25%

0 – 59% F Total 100%

Discussions The Discussion Board is for interacting with your instructor and fellow learners to explore questions and comments related to aerodynamics. It is expected that each student engage in an open and constructive dialogue related to the questions and other discussions. Responses to the weekly discussion questions are required and must be completed within the module dates listed in their respective activities unless modified by your instructor. Your participation in each forum is evaluated on a 0 to 100-pt scale primarily for content indicating analytical thought with a slight emphasis on writing skills to assure interpretability of responses. Exercises Exercises relevant to weekly topics are to be completed at the end of each week and submitted for grading. To assist you in solving and understanding the exercises and their application, common errors and guidance are provided within the assignments. Each exercise assignment is worth 100. Exams The Midterm and Final Examinations consist of multiple choice, computational (formula application), and analysis of theory questions. Both