Aerospace
Aerospace
About aerospace
1～17 item / All 17 items
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Optimization of drone propeller shape
Providing the right products to customers! Introducing the benefits and applications of CAESES at Parrot.
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Optimization of the shape of the volute and diffuser of a centrifugal compressor.
For shape creation, we use CAESES, and for mesh model creation and CFD analysis, we use products from NUMECA!
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Sensitivity approach for turbo pump inducer geometry
Equipped with a function to raise the impeller inlet head by a sufficient amount to prevent excessive cavitation generation!
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Optimization Case of Centrifugal Compressor Impeller Using CAESES
By constructing a parametric model, it is also possible to optimize the entire compressor model!
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Parametric modeling of turbine cooling blades
It is now possible to automatically optimize the cooling structure and cooling performance in conjunction with changes to the blade shape!
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Development of virtual engines utilizing AI
Mainly, CAESES is applied to generate robust parametric models.
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Performance Analysis of Rotor37 Compressor
The analysis results were compared with reference values, and temperature, total pressure, and efficiency were evaluated.
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Reliability analysis of solid fuel rockets
Evaluate the entire process from curing and cooling to transportation and storage, as well as discharge heating and cooling, using AIFEM.
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Topology optimization analysis of aircraft engine turbine disks.
By considering manufacturing constraints, it leads to obtaining an even more ideal shape.
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AICFD M6 Wing Transonic Flow Analysis
The analysis conditions adopt Mach number, angle of attack, and Reynolds number. A comparison of the wing surface pressure coefficient distribution is also conducted.
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[DTEmpower] Strength Evaluation of Spaceship Wall Structure
The data used in this case consists of 500 sets of low fidelity and 100 sets of high fidelity.
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DTEmpower Aircraft Landing Load Prediction
Introduction to data-driven aircraft landing load prediction using data analysis and modeling software.
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TCAE CAA analysis of NACA0012
The mesh model used has eight boundary layers created with TCAE's SnappyHexMesh.
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Optimization of the air intake for AIPOD.
Introduction to parametric modeling using CAD and optimization software CAESES.
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Optimization of compressor blades for aircraft engines
Introduction to the optimization of axial flow compressor blades developed jointly by FRIENDSHIP Corporation and RRD Corporation.
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Optimization of the intake duct for propulsion systems in high Mach number regions.
Payloads, space exploration, and space travel are driving remarkable advancements in the aerospace field.
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Optimization of unmanned aerial vehicles
This paper introduces efforts utilizing optimization algorithms in the design of unmanned aerial vehicles (UAVs), which have seen increasing demand in recent years.
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