Open AccessEffects of forward velocity on noise for a J85 turbojet engine with multi-tube suppressor from wind tunnel and flight tests
Author(s) -
James R. Stone,
J. H. Miles,
N. B. Sargent
Publication year - 1976
Publication title -
the journal of the acoustical society of america
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.619
H-Index - 187
eISSN - 1520-8524
pISSN - 0001-4966
DOI - 10.1121/1.2003103
Subject(s) - wind tunnel , mach number , shroud , noise (video) , supersonic wind tunnel , hypersonic wind tunnel , jet (fluid) , acoustics , jet noise , transonic , jet engine , supersonic speed , nozzle , directivity , range (aeronautics) , aerospace engineering , physics , mechanics , aerodynamics , engineering , structural engineering , computer science , electrical engineering , artificial intelligence , antenna (radio) , image (mathematics)
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