Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Dominique Farcy"'
Publikováno v:
Aerospace Science and Technology
Aerospace Science and Technology, Elsevier, 2019, 90, pp.70-84. ⟨10.1016/j.ast.2019.04.035⟩
Aerospace Science and Technology, 2019, 90, pp.70-84. ⟨10.1016/j.ast.2019.04.035⟩
Aerospace Science and Technology, Elsevier, 2019, 90, pp.70-84. ⟨10.1016/j.ast.2019.04.035⟩
Aerospace Science and Technology, 2019, 90, pp.70-84. ⟨10.1016/j.ast.2019.04.035⟩
International audience; The aim of this paper is to propose an efficient method to evaluate the Added Masses of generic shape bodies in infinite fluid or in the proximity of external walls. The Added Masses (AM) are the result of the inertial reactio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::022b20229d14e9c86609b6df2493b693
https://doi.org/10.1016/j.ast.2019.04.035
https://doi.org/10.1016/j.ast.2019.04.035
Publikováno v:
AIAA AVIATION 2020 FORUM
AIAA AVIATION 2020 FORUM, Jun 2020, VIRTUAL EVENT (RENO), United States. ⟨10.2514/6.2020-3053⟩
AIAA AVIATION 2020 FORUM, Jun 2020, VIRTUAL EVENT (RENO), United States. ⟨10.2514/6.2020-3053⟩
International audience; Experimental measurements, steady (RANS) and unsteady (URANS) numerical simulations are performed on a 3.5:1 prolate spheroid at angles of attack from 0° to 90°. The Reynolds number considered is ReL=2.57*1^6, corresponding
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::75dbee1b7e1f1c0f23de67fcbf7982d8
https://hal.archives-ouvertes.fr/hal-03031977/document
https://hal.archives-ouvertes.fr/hal-03031977/document
Publikováno v:
Journal of Aircraft
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2020, pp.1-16. ⟨10.2514/1.C035882⟩
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2020, pp.1-16. ⟨10.2514/1.C035882⟩
International audience; Reliable prediction of aircraft post-stalled dynamics is entirely dependent on the adequacy of the aerodynamic model. A mathematical model of aerodynamic characteristics of a light aircraft is developed for a wide range of ang
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::df67967dbe914c89c32f55e1a66093a5
https://hal.archives-ouvertes.fr/hal-02475981v2/document
https://hal.archives-ouvertes.fr/hal-02475981v2/document
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
The present paper is devoted to low speed aerodynamics on a 53° swept and twisted blended wing body. The geometry considered is the SACCON configuration, intensively studied in the STO-AVT 161 and 201 working groups. It includes flow control investi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81b4eb976116886c056293d5a293e5d3
https://doi.org/10.2514/6.2014-2391
https://doi.org/10.2514/6.2014-2391
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::97c62dee3d75cb57b64faf4a058bb0f5
https://doi.org/10.2514/6.2014-2393
https://doi.org/10.2514/6.2014-2393
Autor:
Olivier Renier, Dominique Farcy
Publikováno v:
24th Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c6c482c0efb41e92f77350ea85aad74
https://doi.org/10.2514/6.1999-4180
https://doi.org/10.2514/6.1999-4180