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BWB Aircraft Aerodynamic Efficiency Analysis by maheshram2303 is a document available to read on EtoBox.
What is BWB Aircraft Aerodynamic Efficiency Analysis about?
The document presents an aerodynamic analysis of a Blended Wing Body (BWB) aircraft aimed at enhancing fuel efficiency and performance. Utilizing a NASA supercritical airfoil and a 3-D model created in SolidWorks, the study employs Computational Fluid Dynamics (CFD) to evaluate various aerodynamic properties at different angles of attack. Results indicate a maximum lift-to-drag ratio of 15.116 at 0° AOA and a critical AOA of 25°, showcasing improved performance compared to conventional narrow-body airliners
- Author
- maheshram2303
- Language
- EN