Work

Behaviour of Whitcomb Integral Supercritical airfoil at various angles of attack in sonic condition using CFD

Year: 2024

Type: article

Abstract: Understanding the aerodynamic behaviour of an airfoil is crucial for evaluating its performance in generating lift and drag. In this study, the aerodynamic performance of the Whitcomb Integral Supercritical Airfoil is analysed across a range of angles of attack—specifically, 2°, 4°, 6°, 8°, and 10°—under sonic conditions. The primary objective is to investigate and characterize the lift and drag properties exhibited by the airfoil at these various angles of attack. This analysis will provide insights into how the airfoil performs in terms of efficiency and stability at sonic speeds.

Source: International Journal For Multidisciplinary Research

DOI: 10.36948/ijfmr.2024.v06i05.28422

Authors: SHAWN VARGHESE S -, LS MADHUMITHA -

Language: English

Topic: Computational Fluid Dynamics and Aerodynamics

Subfield: Computational Mechanics

Field: Engineering

Domain: Physical Sciences

Open Access status: hybrid

OpenAlex ID: W4403361316

FWCI:

Cites:

Cited by:

Related to: 10