Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Jean Perraud"'
Publikováno v:
Journal of Aircraft
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2018, 54 (2), pp.794-801. ⟨10.2514/1.C033647⟩
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2018, 54 (2), pp.794-801. ⟨10.2514/1.C033647⟩
International audience; Delaying laminar-turbulent transition is considered a crucial issue with respect to the reduction of airplanes environmental impact, allowing to reduce skin friction drag and thus, fuel consumption. As part of this thematic, b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0043db59a46b19c13a26b12efcc2a150
https://doi.org/10.2514/1.c033647
https://doi.org/10.2514/1.c033647
Publikováno v:
Volume 2B: Turbomachinery.
This paper presents an extension of the γ-Rθt~ transition model of Menter et al. (2006) that aims to take into account the effect of a specific type of surface roughness on the transition location. This was done by implementing the roughness transi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d201c4ba77ecef84f8856a2777419f85
https://doi.org/10.1115/gt2017-63237
https://doi.org/10.1115/gt2017-63237
Autor:
Antoine Durant, Jean Perraud
Publikováno v:
Journal of Spacecraft and Rockets
Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics, 2016, 53 (4), p. 730-742. ⟨10.2514/1.A33475⟩
Journal of Spacecraft and Rockets, American Institute of Aeronautics and Astronautics, 2016, 53 (4), p. 730-742. ⟨10.2514/1.A33475⟩
International audience; With the objective of inserting laminar–turbulent transition prediction inside computational fluid dynamics codes (Navier–Stokes solvers and boundary-layer codes), a physically based transition criterion for laminar–turb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::90a50c58a51a02f60d8fa203e09dbcc0
https://hal.archives-ouvertes.fr/hal-01403286
https://hal.archives-ouvertes.fr/hal-01403286
Publikováno v:
Scopus-Elsevier
Laminar-turbulent transition remains a critical issue in a number of cases, including drag reduction, performance prediction of high-lift systems, improved accuracy in general computational fluid dynamics, and reduction of computation cycles for deve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2c9d0c5b96209cad0ecacbbce5780a7d
https://doi.org/10.2514/1.42990
https://doi.org/10.2514/1.42990
Publikováno v:
Journal of Aircraft. 45:1554-1563
Laminar-turbulent transition appears in high-lift configurations through instabilities, attachment-line contamination, or separation. Its prediction may improve the estimation of maximum lift and allows the extrapolation from wind-tunnel measurements
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f4ae2787af9aaf6874117cf47fe89a4
https://doi.org/10.2514/1.32529
https://doi.org/10.2514/1.32529
Publikováno v:
Volume 2B: Turbomachinery.
This paper presents RANS computation results on the highly-loaded low-pressure turbine blade T106C using the Display Formulaγ-Rθt~ transition model. First, a setup methodology is described, addressing key points such as inlet values for the turbule
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58d94443fa96fe6b9598b90baa6f22e1
https://doi.org/10.1115/gt2015-42160
https://doi.org/10.1115/gt2015-42160
Publikováno v:
AIAA Journal. 44:1243-1254
The experimental and numerical transitional interactions in hypersonic flow are studied. The experiments were performed on a hollow cylinder-flare model in the ONERA R2Ch wind tunnel at a Mach number of 5 and for varying stagnation pressure. Wall pre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d400e46685f7bb054292d25d95ea2135
https://doi.org/10.2514/1.10512
https://doi.org/10.2514/1.10512
Publikováno v:
Journal of Aircraft. 41:1183-1190
Performance of transport aircraft in high-lift conditions is directly related to the maximum lift. However, most of the high-lift tests are carried out at subscale conditions, and performance is then derived by extrapolation to flight Reynolds number
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c031ff4706b9e313a5f01668b8aa69a1
https://doi.org/10.2514/1.4297
https://doi.org/10.2514/1.4297
Autor:
Claude Marmignon, Jean Perraud, Michel Lefebvre, Thierry Pot, Ajmal K. Mohamed, Serge Larigaldie, Daniel Pigache, Véronique Joly, Bruno Chanetz, Jean-Luc Vérant, Johan William, Philippe Sagnier, Reynald Bur
Publikováno v:
Aerospace Science and Technology. 4:347-361
This article deals with the research performed in the framework of the internal ONERA Hyperenthalpic Hypersonic Project. This project involved fifteen researchers specialised in different domains, which are the following: fundamental studies on shock
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f5e73d4a52c6302d2c3dcc281f257157
https://doi.org/10.1016/s1270-9638(00)00145-0
https://doi.org/10.1016/s1270-9638(00)00145-0
Publikováno v:
Journal of Aircraft. 35:891-897
Flight tests using a Fokker F100 aircraft equipped with a natural laminar ow glove demonstrated that natural laminar ow is feasible for transport aircraft with up to 130 passengers. Furthermore, the ight tests generated a wealth of experimen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a15addecd88ff25a72d834a13938d37
https://doi.org/10.2514/2.2409
https://doi.org/10.2514/2.2409