Shock Reduction through Opposing Jets—Aerodynamic Performance and Flight Stability Perspectives

Shock Reduction through Opposing Jets—Aerodynamic Performance and Flight Stability Perspectives

In this research paper, investigations of counter flow (opposing) jet on the aerodynamic performance, and flight stability characteristics of an airfoil with blunt leading-edge in supersonic regime are performed. Unsteady Reynolds-Averaged Navier-Stokes (<inline-formula> <math display="...

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Bibliographic Details
Main Authors: Shagufta Rashid, Fahad Nawaz, Adnan Maqsood, Rizwan Riaz, Shuaib Salamat
Format: Article
Language:English
Published: MDPI AG 2019-12-01
Series:Applied Sciences
Subjects:
aerodynamic performance
flow control
opposing jet
flight stability
Online Access:https://www.mdpi.com/2076-3417/10/1/180

Internet

https://www.mdpi.com/2076-3417/10/1/180

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