Work

Analysis of NACA 2412 Airfoil for Aerodynamic Efficiency

Year: 2025

Type: article

Abstract: This research paper focuses on a small foam wing analysis using NACA 2412 airfoil. This study aims to determine the stall angle, the lift coefficient, and the stall speed through theoretical analysis. The findings are essential for understanding the aerodynamic limitations of the wing and for ensuring optimal flight performance.

Source: International Journal for Research in Applied Science and Engineering Technology

DOI: 10.22214/ijraset.2025.67531

Author: Sahil Grover

Language: English

Topic: Aerospace and Aviation Technology

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: diamond

OpenAlex ID: W4408622377

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