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The impact of roughness size on the shock-wave boundary-layer interaction on aero-engine intakes at incidence.
The impact of roughness size on the shock-wave boundary-layer interaction on aero-engine intakes at incidence.
2019
C. Coles
Holger Babinsky
Keywords:
Mechanics
Shock wave
Boundary layer
Surface finish
Materials science
aero engine
Correction
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