Research Article

SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY

Volume: 01 Number: 01 September 10, 2020
EN

SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY

Abstract

In this study, preliminary sizing of a turboprop engine powered high altitude unmanned aerial vehicle and it`s propulsion system for an assumed mission profile in Turkey was performed. Aircraft mission profile is one of the most important design inputs in aircraft design. While the aircraft is dimensioned according to the requirements in the specification (useful payload, range, target cost, etc.), parameters such as cruise altitude and speed within the mission profile affect the engine type, power level, fuel quantity, and therefore the overall dimensions and total weight of the aircraft. The unmanned aerial vehicle with turboprop engine investigated in this study, can stay in the air for at least 24 hours at high altitude (40000 ft) and can be used for border surveillance, coast control, forest fires and land exploration.

Keywords

References

  1. [1] General Atomics Aeronautical Systems, http://www.ga-asi.com/predator-b
  2. [2] https://www.airforce-technology.com/projects/heron-tp-eitan-male-uav/
  3. [3] https://www.baykarsavunma.com/iha-14.html
  4. [4] Raymer, D.P., “Aircraft Design: A Conceptual Approach”, 3rd Edition, 1999.
  5. [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. [6] Mattingly, J., Heiser, W., Pratt, D., Aircraft Engine Design, AIAA Series, 2002.
  7. [7] Kerrebrock J.L., Aircraft Engines and Gas Turbines, MIT, 1984.
  8. [8] P. P. Walsh, P.Fletcher, “Gas Turbine Performance”, 2nd Edition, 2004.

Details

Primary Language

English

Subjects

Aerospace Engineering

Journal Section

Research Article

Authors

Publication Date

September 10, 2020

Submission Date

March 2, 2020

Acceptance Date

July 9, 2020

Published in Issue

Year 2020 Volume: 01 Number: 01

APA
Dinç, A. (2020). SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY. International Journal of Aviation Science and Technology, 01(01), 9-13. https://izlik.org/JA95FS47LN
AMA
1.Dinç A. SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY. IJAST. 2020;01(01):9-13. https://izlik.org/JA95FS47LN
Chicago
Dinç, Ali. 2020. “SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY”. International Journal of Aviation Science and Technology 01 (01): 9-13. https://izlik.org/JA95FS47LN.
EndNote
Dinç A (September 1, 2020) SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY. International Journal of Aviation Science and Technology 01 01 9–13.
IEEE
[1]A. Dinç, “SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY”, IJAST, vol. 01, no. 01, pp. 9–13, Sept. 2020, [Online]. Available: https://izlik.org/JA95FS47LN
ISNAD
Dinç, Ali. “SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY”. International Journal of Aviation Science and Technology 01/01 (September 1, 2020): 9-13. https://izlik.org/JA95FS47LN.
JAMA
1.Dinç A. SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY. IJAST. 2020;01:9–13.
MLA
Dinç, Ali. “SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY”. International Journal of Aviation Science and Technology, vol. 01, no. 01, Sept. 2020, pp. 9-13, https://izlik.org/JA95FS47LN.
Vancouver
1.Ali Dinç. SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY. IJAST [Internet]. 2020 Sep. 1;01(01):9-13. Available from: https://izlik.org/JA95FS47LN

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