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Modeling and Simulations of Aeroacoustic Phenomena of a Launch Vehicle: Boundary Layer Noise and Jet / Shock noise
Modeling and Simulations of Aeroacoustic Phenomena of a Launch Vehicle: Boundary Layer Noise and Jet / Shock noise
Details
Is Active
false
Start Date
July 31, 2002
End Date
Universit di Roma "La Sapienza" / Dip. di Meccanica e Aeronautica
Type
Ricerca Scientifica