Zobrazeno 1 - 5
of 5
pro vyhledávání: '"J. C. S. Lai"'
Publikováno v:
Computational Fluid Dynamics 2004 ISBN: 9783540318002
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a4bfb13b959026ffa2221ca74a6bd1e
https://doi.org/10.1007/3-540-31801-1_43
https://doi.org/10.1007/3-540-31801-1_43
Autor:
John Young, J. C. S. Lai
Publikováno v:
Computational Fluid Dynamics 2002 ISBN: 9783642639388
The flow around a plunging airfoil at Reynolds number Re = 20,000 is simulated with a 2D Navier Stokes solver. At high frequency and low amplitude, lift and thrust of the airfoil are found to agree closely with potential flow solutions produced by an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f492586f762dfb7a7a2bd2b7ca04c5f7
https://doi.org/10.1007/978-3-642-59334-5_39
https://doi.org/10.1007/978-3-642-59334-5_39
Publikováno v:
The Journal of the Acoustical Society of America. 111(3)
Free rotational aerophones such as the bullroarer, which consists of a wooden slat whirled around on the end of a string, and which emits a loud pulsating roar, have been used in many ancient and traditional societies for ceremonial purposes. This ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::99b3d3a68c3e638af52967344c09d0d0
https://pubmed.ncbi.nlm.nih.gov/11931296
https://pubmed.ncbi.nlm.nih.gov/11931296
Autor:
J. C. S. Lai, M. F. Platzer
Presented as Paper 98-0101 at the AIAA 36th Aerospace Sciences Meeting, Reno, NV, 12–15 January 1998 The article of record as published may be found at https://doi.org/10.2514/2.641 Water-tunnel tests of a NACA 0012 airfoil that was oscillated sinu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6699e29698982a0f83aa7729caf688ca
https://hdl.handle.net/10945/70563
https://hdl.handle.net/10945/70563
Publikováno v:
AIAA Journal. 19:673-676
To achieve rapid mixing between a jet flow and its surrounding medium a v is mounted in the jet downstream of the jet nozzle exit. The vane is oscillated in either pitch or plunge by an appropriate excitation mechanism at a constant frequency. The am
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bde29fe2528975577ce9d9b38b083a3c
https://doi.org/10.2514/3.7810
https://doi.org/10.2514/3.7810