Shock Wave Diffraction Phenomena around Slotted Splitters †
Abstract
:1. Introduction
2. Experimental Section
2.1. Shock Tube and Test Section Models
2.2. Schlieren
3. Results and Discussion
3.1. Mach Number of 1.31
3.2. Mach Number of 1.59
4. Conclusions
Acknowledgments
Author Contributions
Nomenclature
AS | Arc of shock |
CS | Contact surface |
LHS | Left-hand side shock wave |
LRES | Last running expansion shock wave |
MDS | Main diffracted shock wave |
MES | Main expansion shock wave |
MSL | Main shear layer |
RHS | Right-hand side shock wave |
SDS | Subordinate diffracted shock wave |
SES | Subordinate diffracted expansion shock wave |
SmSL | Small shear layer |
SubSL | Subordinate shear layer |
SλS | Lambda shocklet structure |
T | Triangular shape |
V | Vortex |
WSW | Weak sound waves |
Conflicts of Interest
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Gnani, F.; Lo, K.H.; Zare-Behtash, H.; Kontis, K. Shock Wave Diffraction Phenomena around Slotted Splitters. Aerospace 2015, 2, 1-16. https://doi.org/10.3390/aerospace2010001
Gnani F, Lo KH, Zare-Behtash H, Kontis K. Shock Wave Diffraction Phenomena around Slotted Splitters. Aerospace. 2015; 2(1):1-16. https://doi.org/10.3390/aerospace2010001
Chicago/Turabian StyleGnani, Francesca, Kin Hing Lo, Hossein Zare-Behtash, and Konstantinos Kontis. 2015. "Shock Wave Diffraction Phenomena around Slotted Splitters" Aerospace 2, no. 1: 1-16. https://doi.org/10.3390/aerospace2010001