Skip to main content

Aircraft Flutter Testing

20020076128 · NASA · 1997

Public domain · NASATechnical Reports

Overview

Wilmer Reed gained international recognition for his innovative research, contributions and patented ideas relating to flutter and aeroelasticity of aerospace vehicles at Langley Research Center. In the early 1980's, Reed retired from Langley and joined the engineering staff of Dynamic Engineering…

Publisher
NASA
Document
20020076128
Year
1997
Pages
1

Key points

  • The DEI Flutter Exciter creates dynamic forces to stimulate structural vibration modes in aircraft during flight testing.
  • It operates on minimal electrical power, avoiding the need for an aircraft's hydraulic system, which reduces cost and complexity.
  • The system is adaptable for various aircraft types, from single-seaters to airliners, and is used worldwide for flutter testing.
  • DEI also provides sub-scale flutter exciters for wind tunnel models, allowing pre-qualification of aircraft designs.
  • The DEI Flutter Exciter is controlled via a digital Cockpit Control Box and powered by DC servo motors.
Frequently asked questions
What is the purpose of the DEI Flutter Exciter?

The DEI Flutter Exciter is designed to create dynamic forces that stimulate structural vibration modes in aircraft during flight testing.

How does the DEI Flutter Exciter benefit aircraft testing?

It operates on very little electrical power, which reduces the need for the aircraft's hydraulic system, thus lowering costs and complexity.

What types of aircraft can use the DEI Flutter Exciter?

The DEI Flutter Exciter is adaptable to a variety of aircraft, including single-seater and airliner-sized vehicles.

Can the DEI Flutter Exciter be used in wind tunnel testing?

Yes, DEI provides sub-scale flutter exciters that can be incorporated into wind tunnel flutter models for pre-qualifying aircraft designs.

How is the DEI Flutter Exciter controlled?

It is controlled directly by the pilot/operator through a digital Cockpit Control Box and Avionics Box electronics and software.

Document

>.. . -

. . . -- I' - . - , S - Transportation

Aircraft Flutter Testing

When activated, the DEI Flutter Exciter alternately slogan for Dynamic Engineering Inc. (DEI) is deflects the airstream upward and downward in a rapid "mobilizing minds and materials in research and manner, creating a force similar to that produced by an development for land, sea, air, and space." That oscillating trailing edge flap. Because the system runs on blend of talent and technology came together in 1972 to very little electrical power, rather than tapping into an establish DEI of Newport News, Virginia. The core of aircraft's hydraulic system, several benefits are realized.

early work by the company was building aircraft models Among them, because the DEI flutter components are a for wind tunnel testing at Langley ~ese&ch Center.

"strap-on" type of hardware, cost and complexity of During his 34-year employment at Langley, Wilmer fitting the system on the aircraft can be lessened. The Reed gained international recognition for his innovative research, contributions and patented ideas relating to DEI Exciter is readily adaptable to a variety of aircraft. It flutter and aeroelasticity of aerospace vehicles. In the is effective on all fued wing and rotorcraft applications, early 1980s, Reed retired from Langley to join the from single-seater to airliner-sized vehicles.

engineering staff of DEI. While at DEI, Reed recognized DEI sub-scale flutter exciters are also available to the need to increase the safety and minimize the cost incorporate into wind tunnel flutter models, permitting and hazards associated with aircraft flight flutter testing. an aircraft builder to pre-qualify a vehicle design.

He thus conceived and patented the DEI Flutter Exciter, In recent years, DEI used its skills to fabricate a now used world wide in flight flutter testing of new or complete set of fan blades for the National Transonic modified aircraft designs. Facility (NTF) at Langley. DEI has applied its ideas on The Flutter Exciter system provides dynamic force suspension techniques to NASA work on large, flexible input to stimulate structural vibration modes of an space structures. More than 1,000 tasks have been aircraft in flight, and through a l l its flying conditions. completed for Langley alone. Employed by NASA This innovative product generates programmed sinusoi- Ames-Dryden, the employee-owned group was also dal forces at controllable frequencies, amplitudes, phases contracted to work on NASKs F-1GXL flight test and sweep durations. By inducing these forces, structural program.

vibrations on the aircraft can be damped. Twenty-five years after creation, DEI has grown to The DEI Flutter Exciter is controlled directly by the several hundred employees with $20 million in annual sales and has expanded its aerodynamic analysis tech- pilotloperator through a digital Cockpit Control Box niques to justify its company claim: "Where imagination and Avionics Box electronics and software. The Exciters takes shape."

are powered by DC servo motors through interconnect- ing cables. Small fued vanes are mounted at the wing tips and tail tips of an aircraft.

Dynamic Engineering Znc. 5 Flutter Exciter mounts at the wing tips and tail tips of an aircraft to damp out structural vibrations.

Source & rights

Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.

Permanent URL — we don’t break links.

Report a problem or request removal

Document details

Doc number
20020076128
Publisher
NASA
Year
1997
Pages
1
File size
239 KB