Flutter Phenomena Effected by The Aerodynamic Load by Abbass Salman

“…Abstract: The basic aim of this project is to define and investigate the flutter condition which occur at the wing and fuselage of the aircraft structure or any flying aerofoil such as engine fins during flight under different conditions and high speeds where the flutter causes a vibration on the wing and fuselage of the aircraft structure also on the structure of the fins which leads to a high risk of structure failure , if these vibrations are not controlled . …”
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Aeroacoustics Assessment of an Hybrid Aircraft Configuration with Rear-Mounted Boundary Layer Ingested Engine by Francesco Petrosino, Mattia Barbarino, Martin Staggat

“…The partial embedding of the engine into the fuselage generates a distortion of the ingested inflow causing additional tonal and broadband BLI noise sources, and, at the same time, alters the existing one, such as the rotor–stator interaction noise (RSI). …”
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STUDY OF THE ELECTROMAGNETIC RESISTANCE OF AN UNMANNED AERIAL VEHICLE UNDER THE ELECTROSTATIC DISCHARGES INFLUENCE by Rustam R. Gaynutdinov, Sergey F. Chermoshentsev

“…The effect of a discharge of static electricity from an engine blade on a UAV fuselage made of a composite material is considered. …”
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Solar UAV : airframe configuration and design by Kurniawan, Juan Septiano.

“…Variations of drag coefficient with respect to change in fuselage radius and length have been investigated in order to meet both the minimum size and drag requirements.…”
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Computational fluid dynamics of unsteady aerodynamic wake on helicopter main rotor-hub assembly by Othman, Nurain

“…Drag force sourced out from the fuselage created 29% to 70% while the rotor produce 30% to 45% of drag. …”
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Multi-Step Structural Optimization Design of Multi-Bubble Pressure Cabin in the Autonomous Underwater Vehicle with Blended-Wing-Body

“…In this paper, multi-bubble pressure cabin is proposed for the flat fuselage of blended-wing-body(BWB) autonomous underwater vehicle(AUV). …”
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Utilizing Dynamic Scattering for Learning Radar Cross-Section of a Flapping-Wing Aircraft by Zeyang Zhou, Jun Huang

“…The aircraft has two rigid wings and a fuselage similar to a bird’s body, where the plane shape of the wing is U-type. …”
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Propeller Slipstream Effect on Aerodynamic Characteristics of Micro Air Vehicle at Low Reynolds Number by Zhaolin Chen, Fan Yang

“…A numerical investigation on propeller-induced flow effects in tractor configurations on a Zimmerman wing-fuselage using the cambered thin airfoil is presented in this paper. …”
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Mathematical Modeling and Stability Analysis of Tiltrotor Aircraft by Hanlin Sheng, Chen Zhang, Yulong Xiang

“…Regarding that, this paper proposes a dividing modeling method which divides a tiltrotor into five parts (rotor, wing, fuselage, horizontal tail, and vertical fin) and to develop aerodynamic models for each of them. …”
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Geometric design and mechanical properties of cylindrical foldcore sandwich structures by Zhou, X, Zang, S, Wang, H, You, Z

“…The design protocol together with the virtual test results can serve as a useful tool for researchers to design cylindrical foldcore sandwich structures for many potential applications including but not limited to aircraft fuselage, submarine shell and other pressurized cylinders. …”

Eco-efficient lightweight carbon-fiber reinforced polymer for environmentally greener commercial aviation industry by Khalil, Y

“…This research aims to perform comparative impact assessment for production of conventional aluminum alloy (AlMg3) used in aircraft fuselage and lighter weight carbon-fiber reinforced polymer (CFRP). …”

Modelling and Simulation in High-Fidelity Crash Analysis of NGCTR-TD Composite Wing by Luigi Di Palma, Mariacristina Nardone, Claudio Pezzella, Marika Belardo

“…This is to alleviate the inertial load acting on the fuselage, thereby protecting occupants from injuries and fire while ensuring the integrity of escape paths. …”
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Optimal damper location for mid-high frequency vibration control on built-up structures: case study using VA one by Abdul Muthalif, Asan Gani

“…The guide to find optimal damper location is tested on a fuselage model of Boeing 737. The fuselage model is developed using VA One software. …”
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Design and Research on Landing Gear Overall Parameters of Pusher Propeller Reconnaissance/Strike UAV by ZHENG Yongfeng, SHEN Junyan

“…The existing specifications and requirements for the overall layout parameter design of aircraft landing gear are mainly applicable to traditional fighters.If the landing gear of pusher propeller reconnaissance/strike unmanned aerial vehicle(UAV)is designed according to these specifications and requirements,it will cause many problems.Proceeding from the layout and flight characteristics of the pusher propeller reconnaissance/strike UAV,a design scheme suitable for the landing gear overall parameters and overall layout of the pusher propeller reconnaissance/strike UAV is proposed by analyzing the definition and connotation of the landing gear overall layout parameters.The takeoff and landing characteristics of the integrated reconnaissance/strike UAV are analyzed.The overall layout parameter of Predator B UAV is compared to verify the effectiveness of the proposed design scheme.The results show that the tail down angle can be reduced,which can be set not less than 6°(static,containing clearance).The turn over angle can be reduced,which can be set within 11°~12°(static).The parking angle can be reduced,which can be set within-2°~-1°.The main landing gear arrangements can choose this type,which is installed onto fuselage of UAV,at extended position,the main landing gear is at the lower side of fuselage,with shape"/\".…”
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Coexistence Analysis Between IMT-2020 and AES operating in L Band on a Final Approach by Luciano Camilo Alexandre, Agostinho Linhares, T. H. Brandão, I. F. da Costa, Arismar Cerqueira S. Jr.

“…We assess the cumulative distribution function (CDF) of interference-over-noise ratio (INR) considering the fuselage attenuation contribution and compare it with the AES protection criteria. …”
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The low sonic boom and aerodynamic optimization with trim constraint of supersonic jet by HAO Xuan, ZHANG Qingqing, SU Cheng, LIU Fang

“…The low sonic boom optimization always make the configuration to a trend of higher swept and longer distribution of the wing along the fuselage，which is unfavorable to the trim and low speed characteristics. …”
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Experimental Investigation of Performance of the Rotorcraft Directional Rudder by Andrej Novák, Karol Ścisłowski, Rafał Kliza, Robert Bąbel, Zbigniew Czyż, Paweł Karpiński

“…The paper presents the results of gyrocopter fuselage experiment testing in a wind tunnel. The model subjected to testing was made in 1:8 scale by 3D printing. …”
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The Effect of Shape of Artificial Ground on Antenna Radiation Pattern by Gabriel Kalapoš, Martin Krchňák, Marek Češkovič, Ján Labun, Michal Schreiner, Tomáš Moravec

“…In naval and aerial transportation, the artificial ground plane is the plane’s fuselage or ship’s hull. Experimental measurements of antenna’s amplitude and phase ratios are presented in the article. …”
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Static analysis of unsteady aerodynamics wake of simplified helicopter model via simulation work by Othman, Nurain, Ishak, Iskandar Shah, Dahalan, Md. Nizam

“…The study also examined the unsteady flow behaviour on the three-dimensional elliptical shape of a fuselage equipped with a rotor hub of the single rotor blade. …”
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Airplane design / by 302711 Roskam, Jan

“…. - Layout design of cockpit, fuselage, wing and empennage : cutaways and inboard profiles -- pt.IV. - Layout design of landing gear and systems -- pt.V. - Component weight estimation -- pt.VI. - Preliminary calculation of aerodynamic, thrust and power characteristics -- pt.VII. - Determination of stability, control and performance characteristics : far and military requirements -- pt.VIII. - Airplane cost estimation : design, development, manufacturing and operating…”