Javascript must be enabled to continue!
Design and Multi-Perspective Investigations on Aeroacoustic Noise Reduction Technologies for Anti-Drone Propeller
View through CrossRef
Abstract
The increasing use of drones in military and defence applications require stealth technology to reduce noise generated by the propeller, which can compromise the drone’s mission. Noise reduction techniques have been developed to address this issue. In this regard, a unique forward speed based drone propeller has been designed. One approach is implementation of optimized sawtooth serrations can be used to reduce noise generated by propellers. The use of serrations on the trailing edge of propeller blades will reduce the noise generated by creating a series of miniature vortices along the trailing edge of the propeller blade, which decrease the intensity of the blade tip vortices and change the frequency of the blade noise. By adjusting the blade angle, the propeller can be optimized to operate at a lower tip speed, reducing noise generated by the blade passing through the air. Numerical simulations using CFD and experimental studies have shown that noise reduction methods in propeller blades can lead to significant reductions in noise, with noise reductions of up to reasonable decibels. According to the calculated model and methods, the most important details are that there are several techniques that can be used to reduce the noise generated by propellers used in defence drones. The combination of these techniques into the design, it is possible to build a stealth drone with a reduced acoustic signature, improved performance, and enhanced mission capabilities for the Anti-Drones to monitor the border areas and counter attack the enemy drones by stealth technology. Through ANSYS Workbench tool, the structural characteristics and aero-acoustics investigations are carried out on this propeller. Through multi-objective investigations, the fine-tuned propeller is shortlisted for hybrid UAV.
American Society of Mechanical Engineers
Title: Design and Multi-Perspective Investigations on Aeroacoustic Noise Reduction Technologies for Anti-Drone Propeller
Description:
Abstract
The increasing use of drones in military and defence applications require stealth technology to reduce noise generated by the propeller, which can compromise the drone’s mission.
Noise reduction techniques have been developed to address this issue.
In this regard, a unique forward speed based drone propeller has been designed.
One approach is implementation of optimized sawtooth serrations can be used to reduce noise generated by propellers.
The use of serrations on the trailing edge of propeller blades will reduce the noise generated by creating a series of miniature vortices along the trailing edge of the propeller blade, which decrease the intensity of the blade tip vortices and change the frequency of the blade noise.
By adjusting the blade angle, the propeller can be optimized to operate at a lower tip speed, reducing noise generated by the blade passing through the air.
Numerical simulations using CFD and experimental studies have shown that noise reduction methods in propeller blades can lead to significant reductions in noise, with noise reductions of up to reasonable decibels.
According to the calculated model and methods, the most important details are that there are several techniques that can be used to reduce the noise generated by propellers used in defence drones.
The combination of these techniques into the design, it is possible to build a stealth drone with a reduced acoustic signature, improved performance, and enhanced mission capabilities for the Anti-Drones to monitor the border areas and counter attack the enemy drones by stealth technology.
Through ANSYS Workbench tool, the structural characteristics and aero-acoustics investigations are carried out on this propeller.
Through multi-objective investigations, the fine-tuned propeller is shortlisted for hybrid UAV.
Related Results
Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
The drone becomes more recognized in the civilian sector; the drone's popularity becomes increases as time goes by. Nevertheless, despite the excitement of flying drones, several t...
Propeller Aerodynamic Design and Optimization
Propeller Aerodynamic Design and Optimization
This research endeavors to illuminate the path toward efficient and optimized propeller design by delving into the realm of aerodynamics. Propellers, as vital mechanical marvels, c...
ACOUSTIC FIELD CHARACTERISTICS UAV SCREW
ACOUSTIC FIELD CHARACTERISTICS UAV SCREW
Unmanned aerial vehicles (UAVs) began to be actively used in civil and military spheres. During flight, UAV nodes emit noise into the environment, while the main radiation node is ...
Deriving Sensitivities of Distributed Propeller Propulsion in Overwing Configuration by using DoE in CFD Simulations
Deriving Sensitivities of Distributed Propeller Propulsion in Overwing Configuration by using DoE in CFD Simulations
In this publication the interaction of propeller and wing of a short haul aircraft concept with distributed propeller propulsion in an over-wing configuration at cruise conditions ...
PEMANFAATAN DRONE UNTUK MONITORING AKURASI PERENCANAAN TAMBANG BATUBARA TERBUKA
PEMANFAATAN DRONE UNTUK MONITORING AKURASI PERENCANAAN TAMBANG BATUBARA TERBUKA
ABSTRAK Pertambangan batubara di Indonesia telah mengalami pasang surut harga yang sangat fluktuatif sejak 2012. Hal tersebut berdampak langsung kepada para pelaku usaha pertambang...
An Energy-Efficient Logistic Drone Routing Method considering Dynamic Drone Speed and Payload
An Energy-Efficient Logistic Drone Routing Method considering Dynamic Drone Speed and Payload
Unmanned aerial vehicle (UAV), or drone is recognized for its potential to improve efficiency and address last-mile delivery issues. As a result, there has been a lot of activity i...
Overview of Wind Tunnel Testing of the Joby Aviation eVTOL Isolated Propeller System
Overview of Wind Tunnel Testing of the Joby Aviation eVTOL Isolated Propeller System
In 2023, Joby Aviation conducted a test of a prototype propeller for an electric vertical takeoff and landing (eVTOL) tilt-propeller aircraft in the 40- by 80-Foot Wind Tunnel at t...
Mechanism of suppressing noise intensity of squeezed state enhancement
Mechanism of suppressing noise intensity of squeezed state enhancement
This research focuses on advanced noise suppression technologies for high-precision measurement systems, particularly addressing the limitations of classical noise reducing approac...

