Cover image for Schlieren Imaging: A Technique to Visualize Supersonic Flow Features
Schlieren Imaging: A Technique to Visualize Supersonic Flow Features
Title:
Schlieren Imaging: A Technique to Visualize Supersonic Flow Features
Author:
Moreto, Jose Roberto
Personal Author:
Publication Information:
Cambridge, MA MyJoVE Corp 2016
Physical Description:
online resource (454 seconds)
Series:
Science Education: Aeronautical Engineering
General Note:
Title from resource description page
Abstract:
Source: Jose Roberto Moreto, Jaime Dorado, and Xiaofeng Liu, Department of Aerospace Engineering, San Diego State University, San Diego, CA Military jet fighters and projectiles can fly at incredible speeds that exceed the speed of sound, which means they are traveling at a supersonic speed. The speed of sound is the speed at which a sound wave propagates through a medium, which is 343 m/s. Mach numbers are used to gauge the flight speed of an object relative to the speed of sound. An object traveling at the speed of sound would have a Mach number of 1.0, whereas an object traveling faster than the speed of sound has a Mach number greater than 1.0. The compressibility effects of air must be accounted for when traveling at such speeds. A flow is considered compressible when the Mach number is greater than 0.3. In this demonstration, Mach 2.0 supersonic flow over a cone will be analyzed by visualizing the formation of shock waves and compression waves in compressible flow using a Schlieren system.
Reading Level:
For undergraduate, graduate, and professional students
Electronic Access:
https://www.jove.com/t/10458
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