Nearfield Unsteady Pressures at Cruise Mach Numbers for a Model Scale Counter-rotation Open Rotor
18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Unsteady boundary-layer induced pressures at high Mach numbers
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Performance of a Mach-Scale Coaxial Counter-Rotating Rotor in Hover
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