Keywords

Aerodynamics; Engineering; Perching; Bird Flight

Abstract

During landing, birds often execute a perching maneuver. The perching maneuver refers to the complex series of actions that birds, and pigeons in particular, will perform when landing. They will typically decelerate by pitching their body to a high angle of attack and spreading their wings. It is believed to help achieve better control and reach optimal lift and drag coefficients. This study seeks to better understand the vortex interactions between the main and tail wings during this maneuver. However, it is still an unexplored phenomenon. Thus, two bird models were conceived to analyze it, one with and one without the tail wing. We tested these two models at a Re = 7500. Synchronous pitching and deceleration motions were performed on the model, mimicking the perching maneuver. Two different accelerations and pitching rates were considered. We used Particle Image Velocimetry (PIV) and force sensor data to compare the velocity field and the forces generated by the model. Due to the vortex interactions between the shed vortices of the main and tail wings, the tail plays a vital role in lift and drag production during the perching maneuver.

Thesis Completion Year

2025

Thesis Completion Semester

Spring

Thesis Chair

Bhattacharya, Samik

College

College of Engineering and Computer Science

Department

Department of Mechanical and Aerospace Engineering

Thesis Discipline

Aerospace Engineering

Language

English

Access Status

Open Access

Length of Campus Access

None

Campus Location

Orlando (Main) Campus

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Rights Statement

In Copyright