The Control Space for Knock Mitigation in Two-Stroke Engines for 10-25 kg Remotely Piloted Aircraft

Authors

Joseph K. Ausserer, USAF Test Pilot School
Marc D. Polanka, Air Force Institute of TechnologyFollow
Paul J. Litke, Air Force Research Laboratory
Jacob A. Baranski, Innovative Scientific Solutions, Inc.

Document Type

Article

Publication Date

9-1-2019

Comments

Copyright © 2019 by ASME

The full text of this article is available via subscription or purchase at the ASME web portal, using the DOI link below.

DOI

10.1115/1.4043745

Source Publication

Journal of Engineering for Gas Turbines and Power

Recommended Citation

Ausserer, J. K., Polanka, M. D., Litke, P. J., & Baranski, J. A. (2019). The Control Space for Knock Mitigation in Two-Stroke Engines for 10-25 kg Remotely Piloted Aircraft. Journal of Engineering for Gas Turbines and Power, 141(9), 091010. https://doi.org/10.1115/1.4043745