Faculty Directory
Dr. Mark Sensmeier
Assistant Professor
Campus: Prescott Campus
College: College of Engineering
Department: Aerospace Engineering
Contact Information:
Embry-Riddle Aeronautical University
3700 Willow Creek Road
Prescott, AZ 86301
Office Building: Bldg 74
Office Location:
Phone: 928-777-3847
E-mail: Mark.Sensmeier@erau.edu
Current Class Schedule:
- AE_304_02PC - Aircraft Structures I
KING ENGINEERING CTR Room 128, Lecture Monday Wednesday Friday 10:20AM - 11:20AM - AE_404_01PC - Aircraft Structures II
Academic Complex 1 Room 104, Lecture Monday Wednesday Friday 10:20AM - 11:20AM - AE_404_02PC - Aircraft Structures II
Academic Complex 1 Room 123, Lecture Monday Wednesday Friday 01:50PM - 02:50PM - ME_305_50PC - Machine Design Lab
Ax Room 122, Laboratory Thursday 01:25PM - 04:05PM - ME_415_01PC - Mdlng & Num. Sim. Enrgy Env Sy
KING ENGINEERING CTR Room 126, Lecture Monday Wednesday Friday 12:40PM - 01:40PM - ME_415_01PC - Mdlng & Num. Sim. Enrgy Env Sy
KING ENGINEERING CTR Room 126, Lecture Monday Wednesday Friday 03:00PM - 04:00PM - UNIV_101_05PC - College Success
Classroom Room 52B, Lecture Tuesday Thursday 12:00PM - 01:00PM
Education:
- PHD in Mechanical Engineering, Virginia Tech
- BS in Aeronautics and Astronautics, Purdue Univ W Lafayette
Publications:
Improved Vibration Monitoring Through Optimization of Sensor Placements, M. D. Sensmeier, K. L. Nichol and T. F. Tibbals, Presented at the 45th ASME International Gas Turbine and Aeroengine Technical Congress, Exposition and Users Symposium, Munich, Germany, May 2000.
Model Integrated Testing for Durability Assessment of Turbine Engines, T. F. Tibbals, M. D. Sensmeier, K. L. Nichol, A. Stoner and C. Biegl, Presented at the ITEA Testing & Evaluation and Science & Technology: Forging Partnerships for the Future of Aerospace Workshop, University of Tennessee Space Institute, Tullahoma, TN, 12-15 Oct 1999.
Assessment of Turbine Engine Structural Integrity Using the Structural Dynamic Response Analysis Code (SDRAC), K. L. Nichol, M. D. Sensmeier, and T. F. Tibbals, Presented at the 44th ASME International Gas Turbine and Aeroengine Technical Congress, Exposition and Users Symposium, 99-GT-410, Indianapolis, IN, 7-10 June 1999.
Application of BladeOPS for Improved Mode Detection, M. D. Sensmeier and K. L. Nichol, Presented at the 4th National High Cycle Fatigue Conference, Monterey, CA, 9-11 Feb 1999.
The Role of Multiaxial Stresses in the Development of Small Fatigue Cracks in Turbine Engine Blades, M. D. Sensmeier and T. F. Tibbals, Proceedings of the Engineering Foundation Small Cracks: Mechanics & Mechanisms Conference, Kahuku, HI, 6-11 Dec 1998.
Development and Application of Tools for Engine Life Monitoring, M. D. Sensmeier, USAF Inaugural Engine Condition Monitoring Workshop, San Diego, CA, 21-23 Oct 1997.
Experimental Validation of Anti-Optimization Approach for Detecting Delamination Damage, M. D. Sensmeier, P. K. Sensharma, R. T. Haftka, O. H. Griffin, Jr. and L. T. Watson, Proceedings of the 36th AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference, New Orleans, LA, April 1995.
External Links:
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