Design and analysis pertaining to the aerodynamic and stability characteristics of a hybrid wing-body cargo aircraft by Ishaan PRAKASH, Prithwish MUKHERJEE

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Strength Analysis of a Rib-Stiffened GLARE-Based Thin-Walled Structure by Andrzej Kubit, Tomasz Trzepieciński, Bogdan Krasowski, Ján Slota, Emil Spišák

Subjects: “…aircraft fuselage skin…”
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Novel Reactive Flex Configuration in Kiwi Wing Foil Surfboard by Adrien M. Fat Cheung, Klaudio Bari

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Skew Bending of Aircraft Fuselage Panels with “L” and “C” Stringers Mounted by Hybrid Joint / Ukośne Zginanie Poszycia Samolotu Z U Sztywnieniami Typu “L” I “C”, Mocowanymi Za Pomocą Złącza Hybrydowego by Sadowski T., Golewski P.

“…A section of fuselage skin with dimension 30 x 200 mm was subjected to numerical study and loaded by skew bending (Fig. 3). …”
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Study of the influence of turbulent flows on the aerodynamic performance of fixed-wing aircraft type UAV MALE by Catalin CUCU, Cristina PUPAZA, Bart JANSSENS, Mihai MIHAILA-ANDRES

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New EoL Routes of Al-Li Aircraft Integral LBW and FSW Welded Panels including New Cr-Free Coatings by Ana Isabel Fernández-Calvo, Clara Delgado, Philippe Dufour, Egoitz Aldanondo, Mario Díaz, María Belén García-Blanco

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Residual Strength Prediction of Aluminum Panels with Multiple Site Damage Using Artificial Neural Networks by Ala Hijazi, Sameer Al-Dahidi, Safwan Altarazi

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Research of Design Technology of Large Opening Lifting Photo-electric Pod by MIAO Zhitao, LI Jianping, BAI Yanjie

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A Structural Design Concept for a Multi-Shell Blended Wing Body with Laminar Flow Control by Majeed Bishara, Peter Horst, Hinesh Madhusoodanan, Martin Brod, Benedikt Daum, Raimund Rolfes

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Experimental and CFD Investigation of Directional Stability of a Box-Wing Aircraft Concept by Gueraiche Djahid, Karpovich Elena, Pikulev Maxim, Kuznetsov Alexander, Sergey Popov, Manoranjan Sinha

“…This study aimed to explore the directional stability issues of a previously studied light box-wing aircraft model with a pusher propeller engine in the fuselage aft section. Earlier configurations have included the use of fuselage together with a lifting system consisting of two wings joined together at their wingtips with vertical stabilizers. …”
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A Method for Calculating Angle of Attack and Sideslip Angle by WEN Qing

“…The wind tunnel test is carried out on the front fuselage model of a large amphibious aircraft,according to the characteristics of the angle of attack sensors on both sides of the fuselage affected by the sideslip angle. …”
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Mutual Aerodynamic Interference Mechanism Analysis of an “X” Configuration Quadcopter by Jianchuan Ye, Jiang Wang, Peijian Lv

“…“Virtual Modes” (VMs) are introduced to examine the mechanisms of aerodynamic interference among the quadcopter’s components (front rotors, rear rotors, and fuselage). By comparing the aerodynamic forces of different VMs, this work shows that mutual interference to the front rotors can be negligible, interference to the rear rotors is due to the wake of front rotors and fuselage, and mutual interference to fuselage is caused by front and rear rotors. …”
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Analysis of the Sound Field Structure in the Cabin of the RRJ-95NEW-100 Prototype Aircraft by Vladimir Lavrov, Petr Moshkov, Dmitry Strelets

“…Wall pressure fluctuation spectrums are obtained for three zones of measuring windows (forward, center, and rear fuselage) in cruising flight mode. The effect of the jet on the pressure fluctuation levels in the tail fuselage is considered. …”
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Research on the Infrared Radiation Suppression of the High-Temperature Components of the Helicopter with an Integrated Infrared Suppressor by Zongyao Yang, Jingzhou Zhang, Yong Shan

“…Installing deflectors at the exhaust port of the fuselage can prevent the detection rays from detecting the high-temperature components inside the fuselage, and when the emissivity of the deflectors is reduced from 0.8 to less than 0.5, or the deflectors are cooled by more than 80 K, they begin to play a role in suppressing the infrared radiation at the bottom of the helicopter.…”
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Imaging and Motion Parameter Estimation of Flying Helicopter With Duo Airborne SARs in <inline-formula><tex-math notation="LaTeX">$X$</tex-math></inline-formula>-Band by Chou-Wei Kiang, Jean-Fu Kiang

“…The velocity vector of fuselage and the spinning rate of main rotors can be accurately estimated, and the spinning rate of the tail rotor can be estimated after removing the strong signals from fuselage and main rotors. …”
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Research on the cantilever roadheader positioning based on near-infrared binocular stereo vision by WANG Xue, ZHOU Hongxu, ZHANG Lei, WANG Huaying

“…The three-dimensional spatial positioning of the roadheader fuselage and the cutting part is realized through image processing and pose calculation. …”
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Research on Aerodynamic Characteristics of Low-speed AerodynamicConfiguration of BWB Analog with and without Ducted Fan by Yang Xiaochuan, Wang Yuntao, Sun Yan, Meng Dehong, Hong Junwu

“…The distribution of pressure coefficient at fuselage and tail had been influenced obviously by ducted fan. …”
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Parameter Sensitivity Study on Inflow Distortion of Boundary Layer Ingested Turbofans by Xin Zhao, Philip Van Hoorn, Hua-Dong Yao, James Alderman

“…The inflow distortion to the fan introduced by the ingestion of the fuselage boundary layer is the most critical challenge in realizing the benefits of boundary later ingesting (BLI) concepts. …”
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Prediction of Aircraft Surface Noise in Supersonic Cruise State by Xiaoguang Zhang, Huixue Dang, Bin Li

“…The jet noise has little effect on the sound pressure level at the front of the fuselage and only contributes to the OASPL at the tail nozzle of the fuselage. …”
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Prediction of Aircraft Surface Noise in Supersonic Cruise State by Xiaoguang Zhang, Huixue Dang, Bin Li

“…The jet noise has little effect on the sound pressure level at the front of the fuselage and only contributes to the OASPL at the tail nozzle of the fuselage. …”
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