An estimate of airframe noise caused by structural vibration
Publication
, Conference
Franzoni, L; Bliss, D
Published in: 6th Aeroacoustics Conference and Exhibit
January 1, 2000
Airframe noise due to structural vibration is estimated. This estimate shows that panel vibration driven by turbulent boundary layer fluctuations can produce airframe noise levels comparable to those measured on aerodynamically "clean" airframe configurations. Although direct radiation from boundary layers is generally agreed to be insignificant, the boundary layer surface pressures can drive the panels to excitation levels that produce significant airframe noise. © 2000 by L. Franzoni and D. Bliss. Published by the American Institute of Aeronautics and Astronautics, Inc.
Duke Scholars
Published In
6th Aeroacoustics Conference and Exhibit
DOI
Publication Date
January 1, 2000
Citation
APA
Chicago
ICMJE
MLA
NLM
Franzoni, L., & Bliss, D. (2000). An estimate of airframe noise caused by structural vibration. In 6th Aeroacoustics Conference and Exhibit. https://doi.org/10.2514/6.2000-2068
Franzoni, L., and D. Bliss. “An estimate of airframe noise caused by structural vibration.” In 6th Aeroacoustics Conference and Exhibit, 2000. https://doi.org/10.2514/6.2000-2068.
Franzoni L, Bliss D. An estimate of airframe noise caused by structural vibration. In: 6th Aeroacoustics Conference and Exhibit. 2000.
Franzoni, L., and D. Bliss. “An estimate of airframe noise caused by structural vibration.” 6th Aeroacoustics Conference and Exhibit, 2000. Scopus, doi:10.2514/6.2000-2068.
Franzoni L, Bliss D. An estimate of airframe noise caused by structural vibration. 6th Aeroacoustics Conference and Exhibit. 2000.
Published In
6th Aeroacoustics Conference and Exhibit
DOI
Publication Date
January 1, 2000