Zobrazeno 1 - 10
of 81
pro vyhledávání: '"B. Chanetz"'
Autor:
R. Bur, B. Chanetz
Publikováno v:
Aerospace Science and Technology. 13:393-401
This article is devoted to the experimental works carried out in the R2Ch blow-down wind tunnel in the framework of the atmospheric re-entry PRE-X demonstrator program and to the fundamental studies performed on a hollow cylinder-flare relative to cr
Autor:
B. Chanetz, G. R. Dehghan Kamaragi
Publikováno v:
2015 World Congress on Sustainable Technologies (WCST).
Iranian wind towers "Badgir" works thanks to natural driving forces, such as differences in temperature between a building and its environment. By evaporation, convection and natural air currents, we can manage the internal thermal comfort of the loc
Design of a boundary layer suction device for a supersonic quiet wind tunnel by numerical simulation
Autor:
B. Chanetz, R. Benay
Publikováno v:
Aerospace Science and Technology. 8:255-271
The paper deals with a numerical contribution for a realization of a quiet supersonic wind tunnel. It is known that upstream of the test-section, acoustic noise originating from the turbulent boundary layer of the nozzle walls has an influence on the
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Publikováno v:
Aerospace Science and Technology. 6:115-121
This action has been undertaken in the framework of a collaborative program between NASA and CNES to support CNES in the development of the Mars Sample Return Orbiter (MSRO). The study, devoted to ONERA in this first phase of the program, consists in
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Publikováno v:
High Temperature Phenomena in Shock Waves
Raymond Brun. High Temperature Phenomena in Shock Waves, Springer, pp.271-298, In press, 978-3-642-25118-4. ⟨10.1007/978-3-642-25119-18⟩
High Temperature Phenomena in Shock Waves ISBN: 9783642251184
Raymond Brun. High Temperature Phenomena in Shock Waves, Springer, pp.271-298, In press, 978-3-642-25118-4. ⟨10.1007/978-3-642-25119-18⟩
High Temperature Phenomena in Shock Waves ISBN: 9783642251184
At very high altitudes, the atmosphere becomes so rarefied that it no longer behaves like a continuous medium when an object is flying in it. As illustrated in Fig.1[1], during re-entry, space vehicles experience rarefied flows in the high-altitude p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7fd41bc2d9d9e775164c98471e9b435d
https://hal-univ-evry.archives-ouvertes.fr/hal-02397840
https://hal-univ-evry.archives-ouvertes.fr/hal-02397840
Autor:
B. Chanetz
Publikováno v:
Progress in Flight Physics.
The paper describes four test-cases around the same configuration type: a hollow cylinder flare model. The first three test-cases are relative to cold hypersonic flow and the fourth one to hot hypersonic flow: (i ) a purely laminar low enthalpy inter
Publikováno v:
Applied Physics B Photophysics and Laser Chemistry. 56:14-20