SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY
Abstract
Keywords
References
- [1] General Atomics Aeronautical Systems, http://www.ga-asi.com/predator-b
- [2] https://www.airforce-technology.com/projects/heron-tp-eitan-male-uav/
- [3] https://www.baykarsavunma.com/iha-14.html
- [4] Raymer, D.P., “Aircraft Design: A Conceptual Approach”, 3rd Edition, 1999.
- [5] Dinc, A. Sizing of a Turboprop Unmanned Air Vehicle and its Propulsion System. Journal of Thermal Science and Technology, 35(2), 53-62, 2015
- [6] Mattingly, J., Heiser, W., Pratt, D., Aircraft Engine Design, AIAA Series, 2002.
- [7] Kerrebrock J.L., Aircraft Engines and Gas Turbines, MIT, 1984.
- [8] P. P. Walsh, P.Fletcher, “Gas Turbine Performance”, 2nd Edition, 2004.
Details
Primary Language
English
Subjects
Aerospace Engineering
Journal Section
Research Article
Authors
Ali Dinç
*
Kuwait
Publication Date
September 10, 2020
Submission Date
March 2, 2020
Acceptance Date
July 9, 2020
Published in Issue
Year 2020 Volume: 01 Number: 01