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                             51 results found
no title author magazine year volume issue page(s) type
1 Accelerated inverse design of vibration isolators with customizable low dynamic stiffness characteristics via deep neural network Hu, Changzhi

82-83 P3 p.
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2 Adaptive neural network based fixed-time attitude tracking control of spacecraft considering input saturation Li, Chengyang

82-83 P3 p.
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3 Aerodynamic and aeroacoustics investigation of tandem propellers in hover for eVTOL configurations Granata, Daniele

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4 Aerodynamics coupling study on the tail cone electrical ducted fan integrated with fuselage Liu, Hanru

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5 Aerodynamics evaluation and flight test of a vertical take-off and landing fixed-wing UAV with joined-wing configuration in transition flight state Baigang, Mi

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6 Aerodynamic shape optimization of a Pterocarya stenoptera seed based biomimetic aircraft using neural network Liu, Chenxi

82-83 P3 p.
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7 Aerodynamic study of a bifurcated turboprop engine inlet with a propeller for flow at ground suction conditions Zheng, Gaojie

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8 An aluminum agglomeration model based on realistic pocket distribution via microcomputed tomography Jiang, Yanfeng

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9 An evaluation strategy of control method for corner separation/stall in compressor cascades Wu, Jianhui

82-83 P3 p.
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10 Application of causal analysis based on systems theory (CAST) to regulatory decision-making: A case study of the Sikorsky S92A Veras Neto, Clementino R.

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11 A preliminary investigation on a novel vortex-controlled flameholder for aircraft engine combustor Zhao, Yuling

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12 A tracking guidance method with funnel scheduling for Mars landing Liu, Yunzhao

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13 Closed-loop AI-aided image-based GNC for autonomous inspection of uncooperative space objects Brandonisio, Andrea

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14 Corrigendum to “External loads identification and shape sensing on an aluminum wing box: An integrated approach” [Aerospace Science and Technology 114 (2021) 106743] Esposito, Marco

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15 Corrigendum to “Numerical Study of Cold Flow Characteristics of a New Integrated Afterburner with Strut Flame Stabilizer” [Aerospace Science and Technology 153C (2024) 109476] Li, Minqiang

82-83 P3 p.
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16 Crashworthiness and stiffness improvement of a variable cross-section hollow BCC lattice reinforced with metal strips Li, Bo

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17 Deep learning-based prediction of initiation jet momentum ratio in jet-induced oblique detonations Bao, Yue

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18 Drag dependency aspects in Hyperloop aerodynamics Radeck, Domenik

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19 Editorial Board
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20 Effect of injection location on mixing characteristics with pylon downstream of cavity Nair, Prasanth P

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21 Effect of local concave non-axisymmetric endwall profiling on endwall secondary flows of a highly-loaded turbine cascade Cao, Zhiyuan

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22 Effects of additional transmission chamber on flow dynamics of a pulsed jet in crossflow Quan, Weimei

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23 Effects of the rotor tip gap on the aerodynamic and aeroacoustic performance of a ducted rotor in hover Goudswaard, Reinier J.

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24 Enhancing the efficiency and energy capacity of the tri-directional FG nanoplate attached to the piezoelectric patch validated by artificial intelligence Yang, Wenqing

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25 Experimental and numerical characterization of E-glass/epoxy plain woven fabric composites containing void defects Siddgonde, Nagappa

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26 Experimental and numerical investigation on the ballistic impact performance of sandwich panels with additively manufactured honeycomb cores Haq, Ahsan Ul

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27 Experimental and numerical investigations into cold flow characteristics of multiple micro-mixing jets for hydrogen-rich gas turbines Chen, Xuanren

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28 Fluid-thermal-structural coupled investigation on rudder leading edge with porous opposing jet in high-speed flow Li, Shaliang

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29 Investigation of the aerodynamic performance of the dragonfly-inspired tandem wings considering the coupling between the stroke plane and phase difference Yang, Xiaojun

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30 Multi-fidelity simulation of inlet mode transition with smooth thrust of turbine based combined cycle Liu, Jun

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31 Multi-objective optimization of the design parameters in longitudinal corrugated tubes to improve crashworthiness performance Koloushani, Mehrdad

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32 Multi-physical fields prediction model for turbine cascades based on physical information neural networks Li, Lele

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33 Multisource data fusion for defect detection in composite additive manufacturing using explainable deep neural network Kumar, Deepak

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34 Non-equilibrium plasma distribution in the wake of a slender blunted-nose cone in hypersonic flight and its effect on the radar cross section Esposito, Salvatore

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35 Nonlinear vibration characteristics and damage detection method of blade with breathing fatigue crack Liu, Yue

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36 Numerical research on flow field structure and droplets distribution of kerosene-fueled rotating detonation ramjet engine Yushan, Zheng

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37 Passive control of flow separation with blade-end slots for a three-stage compressor at different Reynolds numbers Liu, Yangwei

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38 Prediction of pressure distribution and aerodynamic coefficients for a variable-sweep wing Lei, Yuqi

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39 Predictor-corrector reentry guidance for hypersonic glide vehicles based on high-precision analytical solutions Liu, Zhengzhuo

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40 Quasi-static compression response of a novel multi-step auxetic honeycomb with tunable transition strain Wang, Shun

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41 Robust control of Chat-PM: A switched singular system with mode-dependent bounded nonlinearity Han, Chengzhe

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42 Single-mode flutter analysis of drag reduction spike by parameterized eigenvalue method and energy method Huang, Chengde

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43 Static and structural dynamic analysis of thick panel kirigami deployable structures Li, Junlan

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44 Study on concentration distribution and detonation characteristics of typical multiphase fuel in orthogonal flow field Zeng, Linghui

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45 Tension-twist coupling morphing wing using a novel mechanical metamaterial Zhu, Xueren

82-83 P3 p.
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46 Thermal deformation monitoring of large-scale composite honeycomb spaceborne antennas with limited strain measurements Huang, Tianxiang

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47 Trajectory tracking control of a morphing UAV using radial basis function artificial neural network based fast terminal sliding mode: Theory and experimental Derrouaoui, Saddam Hocine

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48 Transient gas path fault diagnosis of aero-engine based on domain adaptive offline reinforcement learning Xu, Jinghui

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49 Uncertainty analysis of rudder shaft thermal conditions on the flutter characteristics of the hypersonic control surface Ye, Kun

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50 Unsteady aerodynamic modeling and flight trajectory simulation of dual-spin projectile based on DNN and transfer-learning Ji, Wen

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51 Wall temperature effects in high-enthalpy supersonic turbulent channel flows considering air dissociation Chen, Xiaoping

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                             51 results found
 
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