Advanced Flight Tests
Instructor(s)
Description
Provides practical knowledge needed to plan a series of flutter envelope expansion tests safely and comprehensively. Includes procedures for post-stall certification and demonstration of new or significantly modified airplane designs to meet civil or military requirements.
Target Audience
Designed for practicing and entry level flight test engineers and managers, aircraft engineers, and aircraft designers.
Fee Includes
Includes instruction, a course notebook, Introduction to Flight Test Engineering, Volumes I and II, by Donald T. Ward, Thomas William Strganac and Rob Niewohner, AGARD Report #776 Aircraft Dynamics at High Angles of Attack, 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: 33 hours • 3.3 CEUs
Course Outline
Day One
- Why such advanced tests? Basic philosophy and attitudes, overview of documents describing governing regulations, history
- Fundamental principles of aeroelasticity: description of static and dynamic aeroelastic phenomena; definitions, terminology, and assumptions; limitations of theory; flutter analysis; development of basic aeroelastic equations; interpretation of supporting analyses
- Experimental and analytical tools used in preflight preparation: modal methods, ground vibration tests and analysis, wind tunnel test techniques, interpretation of dynamically similar wind tunnel model data
Day Two
- Instrumentation for flutter envelope expansion: suitable sensors, near real-time data analysis
- Subcritical response techniques, interpretation of supporting analyses
- Interpreting test results: analyzing real-time data, postflight analysis of data
- Expanding the envelope: excitation methods, clearance to 85% flutter envelopes, example programs
- Discussions of limit cycle oscillations
Day Three
- Foundations of post-stall flight testing: definitions of stall, departure, post-stall gyrations, and spins; description of spin modes and spin phases; development of large disturbance equations of motion; idealized flight path in a spin; balance of aerodynamic and inertial forcing functions; autorotation and its causes; effect of damping derivatives; effect of mass distribution; simplification of post-stall equations of motion
- Aerodynamic conditions for dynamic equilibrium: pitching moment equilibrium, rolling and yawing moment equilibrium; design goals and trends to provide post-stall capability: agility measures of merit, unsteady lift, thrust vector control, vortex control
- Experimental tools for preflight preparation: water tunnel tests and flow visualization tools, static wind tunnel tests, dynamic wind tunnel tests, rotary balance tests
Day Four
- Instrumentation for post-stall flight tests: sensors needed and their specifications; pre-test planning and preparation: data requirements, flight test team preparation and training, flight simulation; maneuver monitoring in real time for envelope expansion
- Emergency recovery devices: types of devices available, sizing and other design constraints, validation
- Subsystem modifications for post-stall testing: additional pilot restraint devices, control system modifications, propulsion system modifications
- Recommended recovery techniques; interpreting post-stall flight test results: analyzing real-time data, postflight analysis of data
Day Five
- Guidelines and discipline for conducting advanced flight tests: test team training, incremental buildup to critical conditions, use of simulation, independent review teams
- Planning for efficiency in data collection and data management: tailoring the scope of the tests to the requirement; identifying critical parts of the envelope; combining maneuvers and integration of backup test points; using all available tools: real-time monitoring, automated inserts; shared data processing between test site and home site
- Contingency planning: attrition of resources, backup support facilities, safety guidelines and documentation; course wrap-up and critique
Comments from Past Participants
"Dr. Ward and Dr. Strganac have a great command of the material and they make the advanced topics in this course much less intimidating." — Chad Woodard, USAF
"Dr. Ward and Dr. Strganac are excellent, intelligent instructors. The presented material was well organized and taught professionally. I would highly recommend to all flight testees." —Ross J. Cooper, Lockheed Martin Aeronautics Company
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
or use the button below:
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
Tools
Email Page
Print Page