A COMPUTATIONAL DETERMINATION OF A NOZZLE ACTIVATED FIXED-WING UAV

This paper proposes new methods and strategies for the propulsion of a mini Unmanned Aerial Vehicle (UAV). Typically, the UAVs are propelled by new technology batteries, fossil fuels, and hybrid systems. An experimental research regarding the usage of compressed air has been carried out. In total 13 nozzles have been installed to the fuselage of the UAV in terms of gaining 3-axis movement during flight. At the end of the manuscript, a MATLAB (Mathworks, US) program is provided in terms of calculating the maximum force and the flying time with the gained force. The UAV, whose design is presented, will be ideal for both defense and border security tasks, as it can move over the vehicle, has extremely high portability, and has a small physical footprint.

Keywords:

Unmanned Aerial Vehicle (UAV), Drag Time to Climb, Take-Off Performance, Maximum Turn Rate,

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1. Ducard, J.J.G., Allenspach, M., “Review of designs and flight control techniques of hybrid and convertible VTOL UAVs”, Aerospace Science and Technology, Volume 118, Pages 1-25, 2021.
2. Dündar, Ö., Bilici, M., Ünler, T., “Design and performance analyses of a fixed wing battery VTOL UAV”, Engineering Science and Technology, an International Journal, Volume 23, Issue 5, Pages 1-12, 2020.
3. Saraçyakupoğlu, T. , Delibaş, H. D. , Özçelik, A. D. "An Experimental Determination and Numerical Analysis Of A Loiter Munition Unmanned Aerial Vehicle System". International Journal of 3D Printing Technologies and Digital Industry, Volume 6, Issue 1, Pages 83-101, 2022.
4. Göv, İ., “Rotor Spacing and Blade Number Effect on the Thrust, Torque and Power of a Coaxial Rotor”, El-Cezerî Journal of Science and Engineering, Volume 7, Pages 487-502, 2020.
5. Raymer, D. P., “Aircraft Design: A Conceptual Approach”, American Institute of Aeronautics and Astronautics-AIAA, Page 273, 1992.
6. Akdeniz, H. Y., “A Study on Aerodynamic Behavior of Subsonic UAVs' Wing Sections with Flaps”, International Journal of Aviation Science and Technology, Volume 02, Issue 01, Pages 22-27, 2021. 7. Anderson, J. D., “Aircraft Performance and Design”, WCB/McGraw-Hill. Boston, Page 453, 1999.
8. Saraçyakupoğlu, T., “The Qualification of the Additively Manufactured Parts in the Aviation Industry”, American Journal of Aerospace Engineering, Volume 6, Issue 1, Pages 1-10, 2019.
9. Saraçyakupoğlu, T. "Abrasive Water Jet (AWJ) Applications in the Aviation Industry", International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), Volume 9, Issue 6, Pages 347-356, 2019.
10. Saraçyakupoğlu, T., "Emniyet İrtifasından Bilgiler: Genel Havacılık, Üretim ve Bakım Süreçleri". ISBN: 978-625-402-030-8, Nobel Academic Publishing, Ankara, Page 55, 2020.
11. Gudmunsson, S., “General Aviation Aircraft Design: Applied Methods and Procedures”, Elsevier, Oxford, Page 21, 2014.
12. Bakar, A., Ke, L., Liu, H., Xu, Z., Wen, D., “Design of Low Altitude Long Endurance Solar-Powered UAV Using Genetic Algorithm”, Aerospace, Volume 8, Issue 228, Pages 1-24, 2021.
13. Novaković, Z., Vasić, Z., Ilić, I., Medar, N., Stevanović, D., “Integration of Тactical - Medium Range UAV and Catapult Launch System”, Scientific Technical Review, Volume 66, Issue 4, Pages 22-28, 2016.
14. Keskin, G., Durmuş, S., Karakaya, M., Teoman, A., Kuşhan, M. C., “Unpowered Flight Principle: Sailplane”, Engineer and the Machinery Magazine, Volume 60, Issue 695, Pages 165-177, 2019.
15. Saraçyakupoğlu, T., "3D Manufacturing Applications in Aviation Industry in Accordance with the Airworthiness Rules And Regulations: A Review". International Journal of 3D Printing Technologies and Digital Industry, Volume 4, Issue 1, Pages 53-65, 2020.
16. Saraçyakupoğlu, T., "Havacılıkta organizasyonel kazalar: B-737 max uçak kazalarının mühendislik perspektifinden incelenmesi ", Mühendis ve Makina, Vol. 61, Issue 701, Pages 241-261, 2020.
17. Saraçyakupoğlu, T., “The Adverse Effects of Implementation of the Novel Systems in the Aviation Industry in Pursuit of Maneuvering Characteristics Augmentation System (MCAS)”. Journal of Critical Reviews, Volume 7, Issue 11, Pages 2530-2538, 2020.
18. Balli, O., Caliskan, H., "On-design and off-design operation performance assessments of an aero turboprop engine used on unmanned aerial vehicles (UAVs) in terms of aviation, thermodynamic, environmental and sustainability perspectives", Energy Conversion and Management, Vol 243, Pages 1-13, 2021.
19. Çabuk, N., “Design and Kinematic Analysis of Proposed Adaptive Landing Gear for Multirotor UAV”, El-Cezerî Journal of Science and Engineering, Volume 9, Issue 1, Pages 159-170, 2022.