Zobrazeno 1 - 10
of 63
pro vyhledávání: '"L. Walpot"'
Autor:
Andrea Scarabosio, Javier Leonardo Araque Quijano, Jorge Tobon, Marco Righero, Giorgio Giordanengo, D. D'Ambrosio, L. Walpot, Giuseppe Vecchi
Hypersonic flight regime is conventionally defined for Mach larger than 5; in these conditions, the flying object becomes enveloped in a plasma. This plasma is densest in thin surface layers, but in typical situations of interest it impacts electroma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1d7c2ea2d12e65a36107d7106b917f2d
http://hdl.handle.net/11583/2963011
http://hdl.handle.net/11583/2963011
Akademický článek
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Publikováno v:
Experiments in Fluids. 50:407-418
The flow-field structure in the vicinity and in the wake of an isolated 3D roughness element has been studied. Different experimental techniques have been coupled and supported by CFD simulation for a good understanding of the flow-field topology. Th
Publikováno v:
Journal of Thermophysics and Heat Transfer
Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics, 2006, 20 (4), pp.663-671. ⟨10.2514/1.20901⟩
Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics, 2006, 20 (4), pp.663-671. ⟨10.2514/1.20901⟩
The present paper focuses on the convective and radiative heat flux predictions required for the post-delta Flight Acceptance Review consolidation of the Huygens entry profile and, in particular, the desired flight path angle at entry interface. This
Publikováno v:
Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences. 357:2249-2278
The paper focuses on the experiments performed in the European high–enthalpy facilities during the crewed space flight hypersonic ground testing technology programme. Emphasis is placed on simple configuration testing enabling validation of the phy
Akademický článek
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Publikováno v:
Journal of Spacecraft and Rockets. 35:107-109
Publikováno v:
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.
The development of a hypersonic characterisation methodology is presented. A boundary layer rake has been design for the in-flight EXPERT project. It is still in an optimisation phase and it accuracy is under evaluation. Based on this experience, ins
Publikováno v:
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.
L.M.G Walpot∗ AOES-Group B.V., Haagse Schouwweg 6G, 2332 KG Leiden, The Netherlands P. Noeding† ASTRIUM Space Transportation GmbH, Huenefeldstr. 1-5, Germany F. Tarfeld‡ DLR Cologne, Linder Hoehe, D-51147 Cologne, Germany R.C. Molina§ ESA-ESTE
Publikováno v:
35th AIAA Thermophysics Conference.