What is it about?
An approximate method for the account of compressibility, which was successfully applied earlier for airfoil with subsonic-type edge, was used for airfoil with supersonic-type edge in the present paper.
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Why is it important?
It has been shown that the value of critical Mach number decreases with increasing the relative thickness of the circular-arc airfoil.
Perspectives
Perspective of this method lies in the possibility calculating the critical Mach number for other forms of airfoils.
Vladimir Alekseevich Frolov
Samara University
Read the Original
This page is a summary of: Critical Mach Number for Flow around Circular-Arc Airfoil, Applied Mechanics and Materials, October 2015, Trans Tech Publications,
DOI: 10.4028/www.scientific.net/amm.798.513.
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