Jeffrey Diebold

Contact Information: 

Email:  dieboj@rpi.edu
Office Phone:  (518) 276-2530
Cell Phone:  (267) 575-1627

Education: 

Received:  Ph.D. in Aerospace Engineering, The University of Illinois, December 2016
Received:  B.S. in Mechanical Engineering, Lehigh University, May 2010

Previous Research Experience:

As a graduate research assistant at The University of Illinois I was involved in a large collaborative effort with The FAA, NASA Glenn Research Center and The University of Washington to experimentally study the effects of leading-edge ice accretion on the aerodynamic performance of swept wings. I conducted numerous wind tunnel studies in The University of Illinois 3-ft x 4-ft Low Speed Wind Tunnel as well as larger scale studies at the 7-ft x 10-ft Walter H. Beech Wind Tunnel at Wichita State University. One of my primary responsibilities within the overall project was the use of five-hole pressure probe wake surveys to better understand the 3D flowfield and aerodynamics of the swept wing with leading-edge ice. My PhD dissertation was focused on understanding the influence of turbulent velocity fluctuations on the measurements of five-hole pressure probes. I quantified turbulence-induced errors in five-hole pressure probe measurements and developed a method to model and correct these errors.

I have also been involved in several other research projects covering a range of topics such as wake bursting in the flowfield of a multi-element airfoil, the unsteady compressible flowfield of an under-expanded jet and the aerodynamics of splitter plates used for wind tunnel testing of semi-span wings. I have experience with numerous experimental methods including surface oil flow visualization, high-speed Schlieren, thermal anemometers, particle imaging velocimetry, pressure sensitive paint and multi-hole pressure probes.

In addition to my research, I have had a considerable amount of teaching experience, including teaching a senior-level course in aircraft performance and stability, mentoring numerous undergraduates in research and working as an instructor in an aerospace engineering summer camp for high school students.

Joined CeFPaC: 
December 2016
Selected Publications: 

Journal Papers:

  • Diebold, J. M. and Bragg, M.B., 2015, "Wake Survey Techinque for Iced Swept Wing Aerodynamics,"  AIAA Journal, Vol. 53, No. 6, pp. 1712-1715.
  • Pomeroy, B.W., Diebold, J.M., Ansell, P.J. and Selig, M.S., 2014, "A Study of Burst Wakes in a Multi-element Airfoil Flowfield,"  AIAA Journal, Vol. 52, No. 4, pp. 821-831.

Conference Papers:

  • Diebold, J.M., Woodard, B.S., Monastero, M.C. and Bragg, M.B., "Experimental Study of Splitter Plates for Use with Semispan Wing Models," AIAA Paper 2015-1227, AIAA Aerospace Sciences Meeting, Kissimmee, FL, January 2015.
  • Diebold, J.M. and Elliott, G., "High-Speed Schlieren Imaging of a High-Speed Jet Impinging on a Flat Plate," AIAA Paper 2014-3094, 44th AIAAn Fluid Dynamics Conference, Atlanta, GA, June 2014.
  • Diebold, J.M., Broeren, A.P. and Bragg, M.B., “Aerodynamic Classification of Swept-Wing Ice Accretion,” AIAA Paper 2013-2825, 5th AIAA Atmospheric and Space Environments Conference, San Diego, CA, June 2013.
  • Pomeroy, B.W., Ansell, P.J., Diebold, J.M. and Selig, M.S., “A Study of Burst Wakes in a Multi-element Airfoil Flowfield,” AIAA Paper 2013-2919, 31st AIAA Applied Aerodynamics Conference, San Diego, CA, June 2013.
  • Broeren, A.P., Diebold, J.M. and Bragg, M.B., “Aerodynamic Classification of Swept-Wing Ice Accretion,” NASA/TM – 2013-216381 also DOT/FAA/TC-13/21.
  • Diebold, J.M. and Bragg, M.B., “Study of a Swept Wing with Leading-Edge Ice Using a Wake Survey Technique,” AIAA Paper 2013-0245, 51st Aerospace Sciences Meeting, Grapevine, TX, January 2013.
  • Diebold, J.M., Aerodynamics of a Swept Wing with Leading-Edge Ice at Low Reynolds Number. M.S. Thesis, Department of Aeronautical and Astronautical Engineering, University of Illinois, Urbana, IL. August 2012.
  • Diebold, J.M., Monastero, M.C. and Bragg, M.B., “Aerodynamics of a Swept Wing with Ice Accretion at Low Reynolds Number,” AIAA Paper 2012-2795, 30th AIAA Applied Aerodynamics Conference, New Orleans, LA, June 2012.