Hailang Zhang

ORCID: 0000-0001-6302-4710
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Research Areas
  • Advancements in Battery Materials
  • Biomimetic flight and propulsion mechanisms
  • Advanced Battery Materials and Technologies
  • Extraction and Separation Processes
  • Advanced Aircraft Design and Technologies
  • Advanced Battery Technologies Research
  • Cavitation Phenomena in Pumps
  • Wind Energy Research and Development
  • Fluid Dynamics and Turbulent Flows
  • Advanced SAR Imaging Techniques
  • Target Tracking and Data Fusion in Sensor Networks
  • Magnetic Properties and Synthesis of Ferrites
  • Remote Sensing in Agriculture
  • Remote Sensing and LiDAR Applications
  • Forest ecology and management
  • Aerospace Engineering and Energy Systems
  • Multimodal Machine Learning Applications
  • High-Temperature Coating Behaviors
  • Ion-surface interactions and analysis
  • Aerodynamics and Fluid Dynamics Research
  • Mineralogy and Gemology Studies
  • Advanced Software Engineering Methodologies
  • Tribology and Lubrication Engineering
  • Semiconductor materials and interfaces
  • Rocket and propulsion systems research

Jiangnan University
2013-2024

Xi'an Jiaotong University
2023-2024

Taiyuan University of Technology
2022-2024

China University of Mining and Technology
2023

Chinese Academy of Sciences
2012-2019

Northwestern Polytechnical University
2015-2019

Technical Institute of Physics and Chemistry
2012

Beijing Information Science & Technology University
2012

Biomass is important in monitoring global carbon storage and the cycle, which quickly accurately estimates forest biomass. Precision forestry modeling place high requirements on obtaining individual parameters of various tree species complex stands, studies have included both overall stand trees. Most existing literature focuses calculating species’ biomass a single stand, there little research stands. This paper calculates stands by combining multispectral light detection ranging (LIDAR)...

10.3390/rs14194715 article EN cc-by Remote Sensing 2022-09-21

ABSTRACT The cycloidal propeller for a Micro-Aerial Vehicle (MAV)-scale cyclogyro in hover was studied using 2D Reynolds-averaged Navier-Stokes equations solver. effects of the blade dynamic stall, parallel Blade Vortex Interaction (BVI), inflow variation and flow curvature were discussed, based on results numerical simulation. from Computational Fluid Dynamics simulation indicated that rotor is actually performing pitching oscillation, if observed moving reference frame. stall vortices shed...

10.1017/aer.2016.38 article EN The Aeronautical Journal 2016-05-10

In recent years, a lot of research work has been carried out on the cycloidal rotors. However, it lacks thorough understanding about effects blade platform shape hover efficiency rotor, and knowledge how to design blades. This paper presents numerical simulation model based Unsteady Reynolds-Averaged Navier–Stokes equations (URANSs), which is further validated by experimental results. The aspect ratio taper are analyzed, shows that rotors with same chord length have quite similar performance...

10.1016/j.cja.2019.01.015 article EN cc-by-nc-nd Chinese Journal of Aeronautics 2019-02-10

10.1016/j.nimb.2012.09.011 article EN Nuclear Instruments and Methods in Physics Research Section B Beam Interactions with Materials and Atoms 2012-09-27

Purpose This paper aims to investigate the mechanisms lying behind cycloidal rotor under hovering status.

10.1108/aeat-10-2015-0222 article EN Aircraft Engineering and Aerospace Technology 2017-11-23

The cycloidal propellers for MAV scale cyclocopter in hovering status were studied this paper based on the URANs solver using 2D, 2.5D, 3D half blade and full model. results from all numerical models validated with experimental results. It was found that 2.5D model cannot produce more accurate than 2D model, hence employed to discuss rotor infinite span. also indicates produces same as but is efficient simulation of finite (3D model) span (2D compared. indicated large pitching amplitude,...

10.2514/6.2016-1350 article EN 54th AIAA Aerospace Sciences Meeting 2016-01-02

The cycloidal propellers for micro aerial vehicle scale cyclocopter in hovering status were studied this paper based on the URANs solver using 2D, 2.5D, 3D half blade and full model. results from all numerical models validated with experimental results. It was found that 2.5D model cannot produce more accurate than 2D model, hence employed to discuss rotor infinite span. also indicated produced same as but efficient simulation of finite (3D model) span (2D compared. large pitching amplitude,...

10.1177/0954410016660218 article EN Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2016-11-08

Purpose This paper aims to investigate the impact of aerofoil camber on performance micro-air-vehicle-scale cycloidal propellers. Design/methodology/approach First, experiments were conducted validate numerical methodology. After that, three turbulent models compared select most accurate one. Then, 2D simulation was carried out 11 aerofoils with different cambers, including five cambered aerofoils, one symmetrical and inverse aerofoils. The are about chord line corresponding ones. Findings...

10.1108/aeat-08-2016-0128 article EN Aircraft Engineering and Aerospace Technology 2018-10-15

Dual layer coatings CrNx and Ni-Fe alloy have been developed for metallic interconnects application by a combined approach. The was deposited on ferritic stainless steel using multi-arc ion plating, the coating electroplated coated subsequently. After oxidation at 800 °C in air 5 h, multi-layer scale composed of NiFe2O4, Cr2O3, Ni-Fe-Cr from outside to inside formed CrNx/substrate with 1.6 μm thick Ni-32 at%Fe coating. Further led decomposition layer, but no pores could be observed near...

10.1016/j.rinp.2019.01.061 article EN cc-by-nc-nd Results in Physics 2019-01-30

Model driven architecture (MDA) is a method which can build abstract model for business logic, and generate the ultimate complete application based on model. Procedure blueprint program process representation describe behavioral of software formally. In this paper, we give Web service development MDA procedure blueprint. This might be useful in with semantic information from extended diagram.

10.1109/icis.2012.71 article EN 2012-05-01

Abstract The numerical simulations for cycloidal propellers based on five aerofoils with different thickness are presented in this paper. CFD simulation is sliding mesh and URANS. results of indicates that all test cases share similar flow pattern. There leading edge vortex trailing-edge due to blade dynamic stall. Interaction between the vortices shed from upstream downstream can be observed. variation relative inflow velocity downwash rotor cage. These factors result large fluctuations...

10.1017/s0001924000010502 article EN The Aeronautical Journal 2015-03-01

Cycloidal rotor is a whose blades pitch around the pitching axis and revolve shaft that parallel to blade. It can generate omni-directional thrust with high efficiency. In this paper, numerical simulation models were validated by wind tunnel experiments. Then physics of cycloidal in forward flight was studied. The effects blade number advance ratio qualitatively discussed based on results. Results analysis indicate more will result smoother force curve, so there be lower vibration. However,...

10.1177/0954410017733290 article EN Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2017-10-09

Accurate estimation of forest individual tree characteristics and biomass is very important for monitoring global carbon storage cycle. In order to solve the problem calculating various species in complex stands, we take terrestrial laser scanning data, unmanned aerial vehicle-laser multispectral data as sources extract spectral characteristics, vegetation index texture height diverse areas through classification species. Based on random (RF) algorithm, extracted features were superimposed...

10.1117/1.jrs.18.014515 article EN Journal of Applied Remote Sensing 2024-02-13
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