Flow Control Using MVG in Shock Wave/Boundary Layer Interaction
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-3379-0_16
Reference32 articles.
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2. Anderson JD (2005) Ludwig Prandtl’s boundary layer. Phys Today 58(12):42–48. https://doi.org/10.1063/1.2169443
3. Ashill PR, Fulker JL, Hackett KC (2001) Research at DERA on sub boundary layer vortex generators (SBVGs). In: 39th aerospace sciences meeting and exhibit. https://doi.org/10.2514/6.2001-887
4. Ashill PR, Fulker JL, Hackett KC (2002) Studies of flows induced by sub boundary layer vortex generators (SBVGs). In: 40th AIAA aerospace sciences meeting and exhibit. https://doi.org/10.2514/6.2002-968
5. Babinsky H, Li Y, Ford CWP (2009) Microramp control of supersonic oblique shock-wave/boundary-layer interactions. AIAA J 47(3):668–675. https://doi.org/10.2514/1.38022
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