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Su Honghua

Researcher at Nanjing University of Aeronautics and Astronautics

Publications -  6
Citations -  276

Su Honghua is an academic researcher from Nanjing University of Aeronautics and Astronautics. The author has contributed to research in topics: Surface integrity & Residual stress. The author has an hindex of 4, co-authored 6 publications receiving 216 citations.

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Grindability and Surface Integrity of Cast Nickel-based Superalloy in Creep Feed Grinding with Brazed CBN Abrasive Wheels

TL;DR: In this paper, the effects of process parameters (i.e., wheel speed, workpiece speed and depth of cut) on the grindability and surface integrity of cast nickel-based superalloys, i.e. K424, during creep feed grinding with brazed cubic boron nitride (CBN) abrasive wheels are investigated.
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Tool Life and Surface Integrity in High-speed Milling of Titanium Alloy TA15 with PCD/PCBN Tools

TL;DR: In this article, the performance and wear mechanism of polycrystalline diamond tools were investigated in high-speed milling of Ti-6.5Al-2Zr-1Mo-1V (TA15) alloy.
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Inverse identification of constitutive parameters of Ti2AlNb intermetallic alloys based on cooperative particle swarm optimization

TL;DR: In this article, a cooperative particle swarm optimization algorithm is developed and implemented into the Matlab programs to identify the enormous constitutive parameters, which can be used for other newly developed metal materials.
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Compressive Strength and Interface Microstructure of PCBN Grains Brazed with High-Frequency Induction Heating Method

TL;DR: In this article, the compressive strength of polycrystalline cubic boron nitride (PCBN) grains was measured using high-frequency induction heating technique, and the results showed that the maximum compressive strengths of brazed grains are obtained in the case of Brazing temperature of 965°C, which does not decrease the original grain strength.
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Neck-spinning quality analysis and optimization of process parameters for plunger components: Simulation and experimental study

TL;DR: A calculable finite element analysis (FEA) model is established to simulate the three-roller neck-spinning process of the plunger component, which includes six typical slipper structures, two roller structures, and two spinning parameters to improve the manufacturing quality of the typical plunger components.