Research and advancements in hybrid airships—A review

M Manikandan, RS Pant - Progress in Aerospace Sciences, 2021 - Elsevier
Abstract Hybrid Airships (HAs) are being touted as an efficient aerial platform for various
applications involving heavy cargo transportation, communications, scientific exploration …

Conceptual design and feasibility study of winged hybrid airship

A Gangadhar, M Manikandan, D Rajaram, D Mavris - Aerospace, 2021 - mdpi.com
In recent years, hybrid airships have been identified as promising alternatives for high
altitude, long endurance missions. In this study, a design methodology to study the feasibility …

Dynamic Stability of the Hybrid Airship Influenced by Added Mass Effect

W Gao, X Yang, J Wang, X Li, B Lin, Y Bi, A Dong - Journal of Aircraft, 2024 - arc.aiaa.org
This paper first derives the second-order approximation of force and moment based on the
definition of added mass and stability derivatives. Further, it establishes a small perturbation …

[HTML][HTML] Wind tunnel testing on a generic model of a hybrid lifting hull

A Ul Haque, W Asrar, AA Omar… - Journal of aerospace …, 2016 - SciELO Brasil
In this research, an experimental investigation was carried out at the International Islamic
University Malaysia-Low Speed Wind Tunnel facility on a generic model of a hybrid lifting …

A Practical Approach for Estimating Drag Increase due to Volume Increase in the Center Body of a High-Speed UAV

U Özdemir - Turkish Journal of Science and Technology, 2024 - dergipark.org.tr
High-speed unmanned aerial vehicles are used for many purposes in aviation. High-speed
aircraft do not only fly at supersonic speed, but their subsonic flight performance is also …

Framework of Conceptual Design Methodology for Hybrid Buoyant Aircraft

AU Haque, W Asrar, AA Omar, E Sulaeman… - Aerotecnica Missili & …, 2016 - Springer
For economic and 'green'transportation, the concept of hybrid buoyant aircraft has recently
become a research focus in the aerospace community. In the present work, a methodology …

Novel efficient wing buoyant aircraft design for enhanced aerodynamic performance

M Hasan - 2021 - etheses.whiterose.ac.uk
The current research aims to design a novel concept for an efficient wing buoyancy assisted
aircraft (EWBA) by investigating the optimum aerodynamic efficiency of next-generation …

Analysis of aerodynamic characteristics for a flying-wing UAV with asymmetric wing damage

B Tan, J Ma, Y Zhang - 2018 33rd Youth Academic Annual …, 2018 - ieeexplore.ieee.org
This paper investigates the influence of aerodynamic characteristics for a flying-wing
Unmanned Air Vehicle (UAV) subject to asymmetric wing damage. Firstly, the conceptual …

[PDF][PDF] Formalization of flight mechanical CS-25 requirements for assessments using flight simulation in preliminary aircraft design

VY Krishnamurthy - 2023 - depositonce.tu-berlin.de
Für die Entwicklung neuer Flugzeuge nutzen Hersteller bereits in frühen Entwurfsphasen
numerische Berechnungsverfahren, die dank der heutigen Rechenleistung immer präziser …

[PDF][PDF] Conceptual Design and Feasibility Study of Winged Hybrid Airship. Aerospace 2022, 9, 8

A Gangadhar, M Manikandan, D Rajaram, D Mavris - 2021 - academia.edu
In recent years, hybrid airships have been identified as promising alternatives for high
altitude, long endurance missions. In this study, a design methodology to study the feasibility …