Thermal Loss Determination for Small Internal Combustion Engines
Document Type
Conference Proceeding
Publication Date
1-13-2014
Abstract
Excerpt: Three analysis techniques were used to measure the heat rejection of a 55 cc air-cooled two-stroke engine. This study was performed as part of a larger effort aimed at extending range and endurance limitations of Group 1 & 2 Remotely Piloted Aircraft (RPA).
Source Publication
52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
Recommended Citation
Rittenhouse, J. A., Rowton, A. K., Polanka, M. D., Ausserer, J. K., Litke, P. J., & Grinstead Jr., K. D. (2014). Thermal Loss Determination for Small Internal Combustion Engines. 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, Session: Air Breathing Propulsion System Integration and Optimization, AIAA 2014-0529. https://doi.org/10.2514/6.2014-0529
Comments
This conference paper is published by AIAA, and is accessible by subscription or purchase using the DOI link on this page.
Author notes:
Joseph Ausserer was an AFIT PhD student at the time of this conference. (AFIT-ENY-DS-16-S-055, September 2016)
Joshua Rittenhouse (AFIT-ENY-14-M-41) and Alexander Rowton (AFIT-ENY-T-14-J-36) were AFIT Masters students at the time of this conference, each graduating in 2014.
Session: Air Breathing Propulsion System Integration and Optimization