Estimation of the damping derivative in pitch for a wedge at supersonic Mach numbers using design of experiments

Shaikh, Javed Shoukat and Kumar, Krishna and Pathan, Khizar Ahmed and Khan, Sher Afghan and Husain, Kharadi Fayaz and Siddiqui, Afreen (2025) Estimation of the damping derivative in pitch for a wedge at supersonic Mach numbers using design of experiments. Journal of Advanced Research in Experimental Fluid Mechanics and Heat Transfer, 18 (1). pp. 106-117. E-ISSN 2756-8202

Preview	PDF (Journal) - Published Version Download (2MB) | Preview
Preview	PDF (Scopus) - Supplemental Material Download (189kB) | Preview

Abstract

This work primarily focuses on numerically modeling the damping derivative over the 2D wedge at different pivot points for considerable values of Mach number and incidence angles. The damping derivative is numerically simulated using regression model analysis. The two-dimensional piston theory of Ghosh is applied to obtain the analytical findings. The current study considers the variables Mach number, wedge angle, and pivot location. In the present investigation, the wedge angle (θ) varies between 2° and 20°, while the Mach number (M) spans 2.2 to 4.0. The results of the damping derivatives are derived by analyzing different Mach numbers (M) and angles of incidence (θ) at various pivot positions (h) ranging from 0.0 to 1.0. This study evaluates the damping derivative results against theoretical predictions, revealing a significant alignment between the two. Both the research findings and the theoretical forecasts show a striking similarity. This research demonstrates that the variation in the damping derivative is influenced by factors like the Mach number (M), wedge angle (θ), and pivot position (h). At each pivot position, the magnitude of the damping derivative decreases with a rise in Mach number, which increases as the angle of incidence increases.

Item Type:	Article (Journal)
Additional Information:	7395/118730
Uncontrolled Keywords:	Mach number, supersonic flow, angle of incidence
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL780 Rockets
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Mechanical Engineering Kulliyyah of Engineering
Depositing User:	Prof. Dr. Sher Afghan Khan
Date Deposited:	25 Jan 2025 12:54
Last Modified:	17 Feb 2025 11:39
URI:	http://irep.iium.edu.my/id/eprint/118730

Actions (login required)

View Item