Aerodynamic Concepts Design Analysis with catia ansys fluent

Explore aerodynamic concept designs and analysis for product design and development in aerodynamics. Apply engineering analysis with workbenches to move toward rapid development of aerodynamic vehicle design and analysis.

Explore fundamental theoretical concepts in elasticity, stress, bending, and fluid dynamics, including lift, drag, thrust, and heat transfer principles essential for aerodynamic design and analysis.

Explore the airplane product development cycle from concept design and modeling to engineering analysis and design changes, emphasizing sketches, parametric modeling, and stability through lift and weight balance.

Develop concept designs for aeroplane structures in Catia by defining cross sections, connecting sections with features, and creating 3D structures using CAD features and guides.

Explore engineering analysis from conceptual design for prototyping through design optimization, applying CFD and finite element analysis with boundary conditions to assess deformation, stresses, and safety.

Develop a fuselage sketch by shaping a rectangular profile, offsetting edges, and constructing geometric elements with parallel lines and control points to ensure an aerodynamically optimized profile.

Create a 3d fuselage by sketching on planes, selecting intersection points, and building circular profiles and lines, isolating features, fixing parts, and converting lines to geometric elements.

Create a 3d fuselage by selecting loft profiles from sketch planes, intersect and isolate points to form circular profiles, then loft front, mid, and rear sections for continuity.

Sketch and assemble a 3D wing by importing aerofoil sections from Excel into Catia V5, scale and position them along x, y, z, and ensure tangency continuity and symmetry.

Develop the vertical and horizontal stabilizers by shaping their surfaces, aligning sections along the airframe, and integrating sketches for design analysis in CATIA and ANSYS Fluent.

Design and assemble a wing mounting structure by sketching a fully constrained plan on multiple planes, fixing mounting points, defining offsets, and creating a smooth, symmetrical wing-fuselage integration.

Perform a fluent cfd analysis in the ANSYS Workbench by importing geometry, assigning aluminum, and running 300 iterations to evaluate drag, lift, and velocity fields over the wing, fuselage, stabilizers.

Open the static structure workbench, set fixed supports, and establish the fluid-structure interface to analyze stress and deformation across the aircraft structure, with results color maps.

Import geometry, set inlet velocity and temperature, initiate the cfd solution, and compute engine thrust in newtons while analyzing streamline flow around the model.

Analyze the engine structural geometry and assemblies in Catia Ansys Fluent, set boundary conditions and pressures, and interpret results to identify maximum values.

Configure boundary conditions and temperature inputs to study heat flux and junction temperatures in an engine thermal analysis, solve the model, and interpret max and min values from the results.