Pitch

Pitch is a fundamental engineering parameter that describes either the spacing between repeated features, such as screw threads or gear teeth, or the angular setting of a component, such as a propeller blade. In threaded and toothed systems, pitch is measured between corresponding points and determines how far a fastener advances or how components engage; in rotating systems, blade pitch changes the angle at which a blade interacts with a fluid. Engineers use pitch to control motion, force transmission, flow, noise, and structural compatibility. Accurate pitch measurements support the design, manufacture, alignment, and performance analysis of mechanical and aerospace systems.

Pitch - Related Videos

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JoVE Science Education - Engineering

Propeller Characterization: Variations in Pitch, Diameter, and Blade Number on Performance

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2023

Source: Shreyas Narsipur, Mechanical and Aerospace Engineering, North Carolina State University, Raleigh, NC A propeller is a twisted airfoil, where the angle of the chord changes with respect to the location, along the radial station, as shown in Figure 1. Propellers are widely used in aircraft and watercraft propulsion systems thereby necessitating detailed characterizations of propellers to design high performance vehicles. Figure 1. Chord, thickness, and pitch at a radial station. One of...

Perceiving Loudness, Pitch, and Location

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2024

The human brain perceives pitch through two primary mechanisms reflected in place theory and frequency theory. Each mechanism describes how sound waves are interpreted as specific pitches by the brain, offering insights into the intricate processes of auditory perception. Place theory, or place coding, suggests that different pitches are heard because various sound waves activate specific locations along the cochlea's basilar membrane. The brain determines the pitch of a sound by identifying...

Aerodynamic Performance of a Model Aircraft: The DC-6B

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2023

Source: Jose Roberto Moreto and Xiaofeng Liu, Department of Aerospace Engineering, San Diego State University, San Diego, CA The low-speed wind tunnel is a valuable tool to study aircraft aerodynamic characteristics and evaluate aircraft performance and stability. Using a scale model of a DC-6B aircraft that has a removable tail and a 6-component external aerodynamic force balance, we can measure the lift coefficient (CL), drag coefficient (CD), pitching moment coefficient (CM), and yaw moment...

Clark Y-14 Wing Performance: Deployment of High-lift Devices (Flaps and Slats)

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2023

Source: David Guo, College of Engineering, Technology, and Aeronautics (CETA), Southern New Hampshire University (SNHU), Manchester, New Hampshire A wing is the major lift-generating apparatus in an airplane. Wing performance can be further enhanced by deploying high-lift devices, such as flaps (at the trailing edge) and slats (at the leading edge) during takeoff or landing. In this experiment, a wind tunnel is utilized to generate certain airspeeds, and a Clark Y-14 wing with a flap and slat...

Multicopter Aerodynamics: Characterizing Thrust on a Hexacopter

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2023

Source: Prashin Sharma and Ella M. Atkins, Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI Multicopters are becoming popular for a variety of hobby and commercial applications. They are commonly available as quadcopter (four thrusters), hexacopter (six thrusters), and octocopter (eight thrusters) configurations. Here, we describe an experimental process to characterize the multicopter performance. A modular small hexacopter platform providing propulsion unit...

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