Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Dustin L. Grissom"'
Autor:
Dustin L. Grissom, Stewart A. L. Glegg, Benjamin S. Smith, W. Nathan Alexander, William J. Devenport
Publikováno v:
Journal of Sound and Vibration. 330:4250-4273
Experiments have been performed on the roughness noise produced by a two-dimensional turbulent wall jet boundary layer flowing over short fetches of sandpaper roughness. A range of rough surface sizes were studied from hydrodynamically smooth through
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdcbafa1ac43f7ff1787a3dad83643b9
https://doi.org/10.1016/j.jsv.2011.03.017
https://doi.org/10.1016/j.jsv.2011.03.017
Autor:
Elisabeth A. Wahl, Stewart A. L. Glegg, William A. Alexander, William J. Devenport, Dustin L. Grissom
Publikováno v:
Journal of Sound and Vibration. 329:3958-3971
This paper introduces a new method for measuring the spectral character of wall pressure fluctuations under turbulent boundary layers by measuring the sound that they radiate in the presence of hydrodynamically smooth sinusoidal ridges in the surface
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6fb3ed07f5b0bea68eae310b0cbc51eb
https://doi.org/10.1016/j.jsv.2010.03.012
https://doi.org/10.1016/j.jsv.2010.03.012
Autor:
Blacksburg Va, Stewart A. L. Glegg, Dustin L. Grissom, Ben Smith, W. Nathan Alexander, William J. Devenport
Publikováno v:
14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference).
Extensive measurements have been made of the roughness noise and wall pressure fluctuations produced by a wall jet boundary layer. Short sandpaper roughness fetches, with grit sizes from 220 to 20 were immersed in a 15 mm thick boundary layer and stu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc4fed00c5ef63039f25fa9b88b39a38
https://doi.org/10.2514/6.2008-2904
https://doi.org/10.2514/6.2008-2904
Publikováno v:
11th AIAA/CEAS Aeroacoustics Conference.
An experimental study has been conducted to determine the low frequency behavior of an unstaggered flat plate cascade. The cascade was excited by a discrete upwash gust with most of its energy below a reduced frequency of 2. The results of this test
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13cc588d05e5b40d374760430c6bd82d
https://doi.org/10.2514/6.2005-2959
https://doi.org/10.2514/6.2005-2959
Publikováno v:
10th AIAA/CEAS Aeroacoustics Conference.
*† A computerized gust generator has been developed and tested for the Virginia Tech Stability Wind Tunnel. The generator consists of 10 airfoil section vanes spanning from the top to the bottom of the tunnel contraction. Computer controlled steppe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a484dc3b13634ab2dca10cb16262ceab
https://doi.org/10.2514/6.2004-2956
https://doi.org/10.2514/6.2004-2956
Publikováno v:
Scopus-Elsevier
This paper considers two alternative mechanisms for sound generation by boundary layers over rough walls. The first mechanism is based on the concept, introduced by Howe, that the hydrodynamic pressure fluctuations in the boundary layer are scattered
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a897973a6bac2c10520a9e557eae4898
http://www.scopus.com/inward/record.url?eid=2-s2.0-84884772077&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-84884772077&partnerID=MN8TOARS
