Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Pao S. Huang"'
Publikováno v:
Journal of Propulsion and Power. 8:1266-1272
The present study demonstrates that the reduced Navier-Stokes code (RNS3D) can be used very effectively to develop a vortex generator installation for the purpose of minimizing the engine-face circumferential distortion by controlling the development
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c6a75a91ce1781d1377164aa5b8e873
https://doi.org/10.2514/3.11472
https://doi.org/10.2514/3.11472
Publikováno v:
10th Applied Aerodynamics Conference.
This paper describes the application of a three dimensional reduced Navier-Stokes code to perform design and analysis of vortex generators on a reengined Boeing 727-100QF center engine inlet S duct. This computer code with vortex generators modeling
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bbce5438f9408116be3d3a3e081735a1
https://doi.org/10.2514/6.1992-2700
https://doi.org/10.2514/6.1992-2700
Publikováno v:
Aerospace Design Conference.
This paper describes the application of a three-dimensional reduced Navier-Stokes code to perform design and analysis of the reengine Boeing 727-100 center engine inlet S duct. This computer code is shown to be cost effective, accurate and easy to us
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::007626ff6d5c51913158670007d4ca2e
https://doi.org/10.2514/6.1992-1221
https://doi.org/10.2514/6.1992-1221
Publikováno v:
30th Aerospace Sciences Meeting and Exhibit.
Computational fluid dynamics was used to investigate the management of inlet distortion by the introduction of discrete vorticity sources at selected locations in the inlet for the purpose of controlling secondary flow. These sources of vorticity wer
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f551e9d8003e1001f3cd755d37c040a5
https://doi.org/10.2514/6.1992-152
https://doi.org/10.2514/6.1992-152