Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Dino Roman"'
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
A computational study was performed for a Hybrid Wing Body configuration that was focused at transonic cruise performance conditions. In the absence of experimental data, two fully independent computational fluid dynamics analyses were conducted to a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3d684431be16f84f191245bf77158c6a
https://doi.org/10.2514/6.2016-0266
https://doi.org/10.2514/6.2016-0266
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
A model problem, based on the NACA0012 airfoil, is studied. The thickness distribution of the symmetric NACA0012 airfoil is optimally approximated with a 4 th -order Bezier curve. This best-fit approximation is designated Bez4-0012. Introducing this
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64557b3a6db0107d09f6bbe8a9256f5a
https://doi.org/10.2514/6.2011-3176
https://doi.org/10.2514/6.2011-3176
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
A Mach 0.93 Blended-Wing-Body (BWB) configuration was developed using CFL3DV6, a Navier-Stokes computational fluid dynamics (CFD) code, in conjunction with the Wing Multidisciplinary Optimization Design (WingMOD) code, to determine the feasibility of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::73d97f9096b4a7f74cd27f9220af3e69
https://doi.org/10.2514/6.2003-554
https://doi.org/10.2514/6.2003-554
Publikováno v:
9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecac6b3dc4373386be82b863071aaca5
https://doi.org/10.2514/6.2002-5666
https://doi.org/10.2514/6.2002-5666