TY  - CONF
AU  - Hasan, Mohammad Sakib
AU  - Svorcan, Jelena
AU  - Tanović, D.
AU  - Baş, G.
AU  - Durakbasa, Numan M.
PY  - 2021
UR  - https://machinery.mas.bg.ac.rs/handle/123456789/3683
AB  - High altitude platforms or Pseudo-satellites (HAPS) are unmanned aerial vehicles that can fly above 17 km from sea level. It can take advantage of weak stratospheric winds and solar energy to operate without interfering with current commercial aviation and with enough endurance to provide long-term services as satellites do. The technological innovations and the growing urgency to expand the availability of broadband led to the development of HAPS. Besides that, Earth observation, positioning, astronomy, and science are the main applications of High altitude platforms, or Pseudo-satellites (HAPS). In this paper, the conceptual design of the novel HAPS UAV based on the initial requirements regarding cruising height of 20 km, the cruising velocity of 25 m/s, and payload of 15 kg were performed and described. The HAPS wing was defined and aerodynamically studied in detail. The computed nominal load was used as input parameter for structural analysis of the wing’s inner structure comprising outer shell, main spars, and ribs made of composite and plastic materials. All computations were performed using commercial software package ANSYS. The obtained results are discussed and graphically presented by computed stress and deformation fields.
PB  - Springer Science and Business Media Deutschland GmbH
C3  - Lecture Notes in Mechanical Engineering
T1  - Conceptual Design and Fluid Structure Interaction Analysis of a Solar Powered High-Altitude Pseudo-Satellite (HAPS) UAV Wing Model
EP  - 105
SP  - 93
DO  - 10.1007/978-3-030-62784-3_8
ER  - 

@conference{
author = "Hasan, Mohammad Sakib and Svorcan, Jelena and Tanović, D. and Baş, G. and Durakbasa, Numan M.",
year = "2021",
abstract = "High altitude platforms or Pseudo-satellites (HAPS) are unmanned aerial vehicles that can fly above 17 km from sea level. It can take advantage of weak stratospheric winds and solar energy to operate without interfering with current commercial aviation and with enough endurance to provide long-term services as satellites do. The technological innovations and the growing urgency to expand the availability of broadband led to the development of HAPS. Besides that, Earth observation, positioning, astronomy, and science are the main applications of High altitude platforms, or Pseudo-satellites (HAPS). In this paper, the conceptual design of the novel HAPS UAV based on the initial requirements regarding cruising height of 20 km, the cruising velocity of 25 m/s, and payload of 15 kg were performed and described. The HAPS wing was defined and aerodynamically studied in detail. The computed nominal load was used as input parameter for structural analysis of the wing’s inner structure comprising outer shell, main spars, and ribs made of composite and plastic materials. All computations were performed using commercial software package ANSYS. The obtained results are discussed and graphically presented by computed stress and deformation fields.",
publisher = "Springer Science and Business Media Deutschland GmbH",
journal = "Lecture Notes in Mechanical Engineering",
title = "Conceptual Design and Fluid Structure Interaction Analysis of a Solar Powered High-Altitude Pseudo-Satellite (HAPS) UAV Wing Model",
pages = "105-93",
doi = "10.1007/978-3-030-62784-3_8"
}

Hasan, M. S., Svorcan, J., Tanović, D., Baş, G.,& Durakbasa, N. M.. (2021). Conceptual Design and Fluid Structure Interaction Analysis of a Solar Powered High-Altitude Pseudo-Satellite (HAPS) UAV Wing Model. in Lecture Notes in Mechanical Engineering
Springer Science and Business Media Deutschland GmbH., 93-105.
https://doi.org/10.1007/978-3-030-62784-3_8

Hasan MS, Svorcan J, Tanović D, Baş G, Durakbasa NM. Conceptual Design and Fluid Structure Interaction Analysis of a Solar Powered High-Altitude Pseudo-Satellite (HAPS) UAV Wing Model. in Lecture Notes in Mechanical Engineering. 2021;:93-105.
doi:10.1007/978-3-030-62784-3_8 .

Hasan, Mohammad Sakib, Svorcan, Jelena, Tanović, D., Baş, G., Durakbasa, Numan M., "Conceptual Design and Fluid Structure Interaction Analysis of a Solar Powered High-Altitude Pseudo-Satellite (HAPS) UAV Wing Model" in Lecture Notes in Mechanical Engineering (2021):93-105,
https://doi.org/10.1007/978-3-030-62784-3_8 . .