# Earl H. Dowell

William Holland Hall Distinguished Professor

Professor Dowell's principal teaching interest and research activity is in the field of aeroelasticity - which is the study of the dynamic interaction between an aerodynamic flow and an elastic structure, such as aircraft wings in high speed flight, long span bridges and tall buildings responding to wind loadings, or airflow through the mouth and lungs. Dr. Dowell has also done research in acoustics, nonlinear dynamics, structural dynamics, and unsteady aerodynamics.

Professor Dowell's major research accomplishments include the first definitive research monograph on the aeroelasticity of plates and shells, the first derivation and solution of the nonlinear equations of motion for a helicopter rotor blade (the Hodges-Dowell equations), and work with Professor Kenneth Hall and several graduate students and post-doctoral fellows on reducing the dimensions of mathematical models for very complex high-dimensional fluid/structural systems. Professor Dowell teaches undergraduate and graduate courses on dynamics and aeroelasticity.

Here are seven short videos showing experimental aeroelastic models undergoing limit cycle oscillations in the Duke wind tunnel.

1. An airfoil with a nonlinear freeplay in the connection from the main airfoil to the trailing edge control surface.
2. A delta wing with a strong structural nonlinearity as a result of tension in the mid-plane of the plate-like wing induced by bending of the wing out of its initially undeformed plane.
3. A very high aspect ratio wing that behaves as a beam with double bending (both transverse to and in-line with the aerodynamic flow field) and twisting. A nonlinear coupling among double bending and twisting occurs. Also the aerodynamic flow field experiences separation due to the large motions involved.
4. A delta wing with an external store, flutter and limit cycle oscillations.
5. LCO and Flutter of WingStore model
6. Flapping Flag Flutter
7. LCO of Cropped Delta Wing In the video you will see a cropped delta wing (that simply means we cropped off that would otherwise be a delta or triangular wing). The wind speed in the wind tunnel is shown by the dial in one of the frames. In the other two frames you see signals from two strain gauge bridges, bending and torsion, and of course the wing itself.
The wind speed at which flutter is predicted to occur theoretically is about 19 meters/second. The experimental flutter speed based on observation of the strain gauge signals is about 21 meters/second. Note that at the wind speed when flutter starts, both strain gauges show dominant response at a frequency of 12 Hz. This large peak at a single frequency is a characteristic identifier of flutter. Also note that the motion of the wing is not easily visible to the eye until a higher wind speed in the range of 24-26 meters/second and the motion is most visible at the wing tip. Once the flutter speed is exceeded, limit cycle oscillations occur due a strong structural nonlinearity.
8. Experimental Aeroelastic Models: Design and Wind Tunnel Testing for Correlation with New Theory - An overview of Wind Tunnel Testing in Duke University

## Appointments and Affiliations

• William Holland Hall Distinguished Professor
• Professor in the Thomas Lord Department of Mechanical Engineering and Materials Science
• Affiliate of the Duke Initiative for Science & Society

## Contact Information

• Office Location: 185 Hudson Hall, Box 90300, Durham, NC 27708
• Office Phone: +1 919 660 5321
• Websites:

## Education

• B.S. University of Illinois, 1959
• Sc.M. Massachusetts Institute of Technology, 1961
• D.Sc. Massachusetts Institute of Technology, 1964

## Research Interests

Aeroelasticity, acoustics, nonlinear dynamics, structural dynamics, and unsteady aerodynamics.

## Awards, Honors, and Distinctions

• Den Hartog Medal. ASME. 2009
• Daniel Guggenheim Medal. American Institute of Aeronautics and Astronautics. 2009
• Spirit of St. Louis Medal. American Society of Mechanical Engineers. 2008
• Walter J. and Angeline H. Crichlow Trust Prize. American Institute of Aeronautics and Astronautics. 2007
• Honorary Fellow. AIAA. 2004
• Theodore von Karman Lectureship Award. American Institute of Aeronautics and Astronautics. 2001
• Distinguished Service Award. American Academy of Mechanics. 1994
• Board of Governors. Research Triangle Institute. 1994
• Elected Member. National Academy of Engineering. 1993
• Fellow. American Society of Mechanical Engineers. 1993

## Courses Taught

• ME 775: Aeroelasticity
• ME 592: Research Independent Study in Mechanical Engineering or Material Science
• ME 591: Research Independent Study in Mechanical Engineering or Material Science
• ME 541: Intermediate Dynamics: Dynamics of Very High Dimensional Systems
• ME 494: Engineering Undergraduate Fellows Projects
• ME 493: Engineering Undergraduate Fellows Projects
• ME 492: Special Projects in Mechanical Engineering
• ME 491: Special Projects in Mechanical Engineering
• ME 392: Undergraduate Projects in Mechanical Engineering
• ENERGY 796T: Bass Connections Energy & Environment Research Team
• ENERGY 795T: Bass Connections Energy & Environment Research Team
• ENERGY 396T: Bass Connections Energy & Environment Research Team
• ENERGY 395T: Bass Connections Energy & Environment Research Team
• EGR 244L: Dynamics
• CEE 625: Intermediate Dynamics: Dynamics of Very High Dimensional Systems

## Representative Publications

• Latif, U., E. H. Dowell, E. Uddin, M. Y. Younis, and H. M. Frisch. “Comparative analysis of flag based energy harvester undergoing extraneous induced excitation.” Energy 295 (May 15, 2024). https://doi.org/10.1016/j.energy.2024.130995.
• Varigonda, S. V., L. P. Serafim, M. Freydin, E. H. Dowell, and V. Narayanaswamy. “Two-dimensional pressure field imaging of an elastic panel executing post-flutter oscillations.” Journal of Fluids and Structures 125 (March 1, 2024). https://doi.org/10.1016/j.jfluidstructs.2023.104056.
• Dowell, E. H. “Coupled-Mode Versus Single-Degree-of-Freedom Flutter: The Third Parameter in Flutter.” AIAA Journal 62, no. 2 (February 1, 2024): 864–68. https://doi.org/10.2514/1.J063255.
• He, Y., A. Shi, E. H. Dowell, and X. Li. “Correction: Panel Aeroelastic Stability in Irregular Shock Reflection (AIAA Journal Vol. 60, No. 11, 10.2514/1.J061902).” AIAA Journal 62, no. 2 (February 1, 2024): AU1–2. https://doi.org/10.2514/1.J061902.c1.
• He, Y., A. Shi, and E. H. Dowell. “Panel Aeroelastic Hysteresis Induced by Shock-Reflection Transition.” AIAA Journal 62, no. 1 (January 1, 2024): 418–27. https://doi.org/10.2514/1.J063554.