Principles of Aerospace Engineering
Instructor(s)
Description
The objective of this course is to provide an overview and integrated exposure to airplane aerodynamics, performance, propulsion, flight mechanics, mass properties, structural dynamics, aeroelasticity, structural loads, structures, ground testing, flight testing and certification. The material presented in this course is in the form of lecture notes and showing examples of the Basic Aerospace Engineering software. This course shows the relationship between aircraft certification requirements, engineering analysis and testing.
Target Audience
This course is intended as an overview for non-aerospace engineering-degreed professionals, managers, military and government personnel who are involved in aircraft design and certification.
Fee Includes
Includes instruction, a course notebook, Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control, by Thomas R. Yechout, a copy of Basic Aerospace Engineering software, refreshments and five lunches. The course notes are for participants only and are not for sale.
Fees: See fee information for individual classes in the registration column on the right side of this page.
Class Time
Class time: 31.5 hours • 3.15 CEUs
Course Outline
Day One
- Introduction
- Atmospheric models and airspeed measurements
- Introduction to certification requirements
- Introduction to aerodynamics—review of basic aerodynamic concepts: airfoil fundamentals, finite wings, aircraft aerodynamics. Overview of wind tunnel testing, overview of computational fluid dynamics methods
- Introduction to propulsion—types of propulsion systems, thrust calculations
- Airplane performance—review basic airplane performance theory; airspeeds, takeoff, landing and cruise performance; climb performance; turning performance, range, and endurance
Day Two
- Weight and balance—calculation of mass properties: weight, center of gravity and moment of inertia; establishing the weight-cg envelope
- Flight mechanics—aircraft axis systems, aircraft equations of motion, static and lateral-directional stability, longitudinal and lateral-directional applied forces and moments. Linearizing the equations of motion; aircraft dynamic stability
- Mechanics of materials—material behavior under loading, stress-strain relations, beam bending and buckling, yield, compressive, tensile and fatigue strengths
Day Three
- Mechanical vibrations and structural dynamics
- Aeroelasticity—static aeroelasticity: divergence, control effectiveness, reversal; dynamic aeroelasticity: gust response, flutter, and buffet
- Structural loads—external loads classifications; V-n diagram; structural design airspeeds derivations; balanced maneuver loads, pitch maneuvers loads, roll maneuver loads, yaw maneuver loads
Day Four
- Structural loads—gust loads, landing loads, ground loads, fatigue loads, wing loads, horizontal tail loads, vertical tail loads, fuselage loads, control surface loads, and miscellaneous loads
- Aircraft structures—structural design concept, static strength design, factor of safety, material selection, introduction to the finite element method, damage tolerance design. Historical context of safe life, fail safe and damage tolerance
- Ground testing: instrumentations, bird strike, landing gear drop test, ground vibration, ground loads calibration, static loads tests, and fatigue loads tests
- Flight testing : instrumentations, stall speeds, operational speeds, longitudinal stability and control, directional stability and control, flutter, flight loads validation, operational loads monitoring
Day Five
- Certification—certification agencies, certification process, how to show compliance
- Airplane design—design requirements and objectives, design optimization
- Airplane crashes—what went wrong, why, structural failure, engine failure, landing failure, loss of control
- Summary
Dates and Locations
For Course Information
Contact Kim Hunsinger
at 785-864-4758
or use the button below:
On-Site Course Information
Find out how courses
can be tailored to
your company’s needs.
Contact Soma Chakrabarti
at 785-864-7855
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Registration Information
Mail
Aerospace Short Courses
The University of Kansas
Continuing Education
Registrations
1515 St. Andrews Drive
Lawrence, KS 66047-1625
Phone
Toll-free 877-404-5823
or 785-864-5823
Fax
785-864-4871
TDD
800-766-3777
E-mail
kuce@ku.edu
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