Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Andres Canchero"'
Publikováno v:
AIAA Journal. 54:3778-3786
A nonintrusive measure of the exhaust plume and immediate sound field produced by a cluster of two thrust-optimized parabolic contour nozzles is studied during two steady-state conditions. The first condition is at a nozzle pressure ratio of 25, at w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2e6fd9d10aa6312c6cf2b480dbe207e
https://doi.org/10.2514/1.j055053
https://doi.org/10.2514/1.j055053
Publikováno v:
AIAA Journal. 54:1660-1669
The plume produced by a cluster of two large-area-ratio thrust-optimized parabolic contour nozzles is visualized over a range of nozzle pressure ratios by way of retroreflective shadowgraphy. Both nozzles exhibit free-shock separated flow, restricted
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc979b08e6e2ac6af24dc13b6ae272fe
https://doi.org/10.2514/1.j054622
https://doi.org/10.2514/1.j054622
Autor:
Juan Pedro Monteagudo, Juan Sebastián Delnero, Julio Marañón Di Leo, Andres Canchero, Iban Echapresto Garay
Publikováno v:
Anales AFA. 23:17-20
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::274d489a8cb30660e40630b875f095c1
https://doi.org/10.31527/analesafa.2013.23.3.17
https://doi.org/10.31527/analesafa.2013.23.3.17
Publikováno v:
Whither Turbulence and Big Data in the 21st Century? ISBN: 9783319412153
The vibro-acoustic loads produced by a cluster of two large area ratio thrust optimized parabolic contour nozzles are studied over a range of pressure ratios encompassing free-shock separated flow, restricted shock separated flow, and the end-effects
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::825496c4211be37d46bc99ae5d40d2b0
https://doi.org/10.1007/978-3-319-41217-7_8
https://doi.org/10.1007/978-3-319-41217-7_8
Autor:
Ana Elena Scarabino, Andres Canchero, Federico Bacchi, Mariano Oscar García Saínz, J. Sebastian Delnero
This work experimentally and numerically analyzes the flow configurations and the dynamic wind loads on panels of rectangular L/h 5:1 cross section mounted on a structural frame of rectangular bars of L/h 0.5:1, corresponding to a radar structure. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b975b17bb1b91cdca71994baa05757be
http://koreascience.or.kr/article/ArticleFullRecord.jsp?cn=KJKHCF_2016_v23n1_1
http://koreascience.or.kr/article/ArticleFullRecord.jsp?cn=KJKHCF_2016_v23n1_1
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
This paper presents an experimental analysis of the effect known as “double stall” or “dynamic stall” of an airfoil under incident turbulent flow conditions. In particular, it has been used a Wortmann FX 63-137 airfoil, which is largely used
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::340ab5a1c3d43f018db06f4dd355ee95
https://doi.org/10.2514/6.2014-2993
https://doi.org/10.2514/6.2014-2993