Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Cebeci–Smith model"'
Publikováno v:
Journal of Thermophysics and Heat Transfer. 33:216-224
A database of heating and pressure measurements on a 7 deg half-angle cone in a high-enthalpy expansion tunnel in CO2 has been generated to support development and validation of computational model...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6ee91cd3a949a0b3d38629e3baaf0a56
https://doi.org/10.2514/1.t5472
https://doi.org/10.2514/1.t5472
Autor:
Romit Maulik, Omer San
Publikováno v:
International Journal of Computational Fluid Dynamics. 31:69-92
This paper puts forth a dynamic framework for investigating the subgrid scale physics of decaying two-dimensional turbulence utilising a modular approach with eddy viscosities in various functional forms. The derivation of the low-pass spatially filt
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81c24c9d8bd59f1ade9894fa165504ab
https://doi.org/10.1080/10618562.2017.1287902
https://doi.org/10.1080/10618562.2017.1287902
Publikováno v:
AIAA Journal. 54:2721-2733
High-order methods have demonstrated their potential in large-eddy simulations of turbulent flows with relatively low Reynolds numbers. The cost becomes a serious limiting factor for high-Reynolds-number problems. A promising approach to reduce the c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d1565ae8bfb0c3e6527d911aa7de458
https://doi.org/10.2514/1.j054826
https://doi.org/10.2514/1.j054826
Akademický článek
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Publikováno v:
Journal of Spacecraft and Rockets. 50:69-95
Simulations of a shock emanating from a compression corner and interacting with a fully developed turbulent boundary layer are evaluated herein. Mission-relevant conditions at Mach 7 and Mach 14 are defined for a precompression ramp of a scramjet-pow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc69683ae50f29f31b4cffedad362bd6
https://doi.org/10.2514/1.a32250
https://doi.org/10.2514/1.a32250
Publikováno v:
Journal of Aircraft. 47:805-811
thus alleviating the grid-spacing dependency found in other detached eddy simulation and hybrid Reynoldsaveraged Navier–Stokes and large eddy simulation models. Within the hybrid Reynolds-averaged Navier–Stokes andkinetic eddy simulation model, f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::05fed22dfa580e08ec3500b0435865f3
https://doi.org/10.2514/1.43454
https://doi.org/10.2514/1.43454
Autor:
Johan C. Kok
Publikováno v:
AIAA Journal. 38:1292-1295
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a5bbac420f807330bb62bab7b8879b9
https://doi.org/10.2514/2.1101
https://doi.org/10.2514/2.1101
Autor:
Giuseppe Mingione, Vincenzo Brandi
Publikováno v:
Journal of Aircraft. 35:240-246
The aim of this paper is to present the Italian icing computational environment code, I 2 CE, developed by CIRA, and discuss its evaluation for ice accretion on single and multielement airfoils. The aerodynamic module of the code is based on a potent
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::95584bdbcc0aefea18b26a0d12ddca24
https://doi.org/10.2514/2.2290
https://doi.org/10.2514/2.2290
Autor:
M. Olcmen, Roger L. Simpson
Publikováno v:
AIAA Journal. 31:1545-1554
~'vw/(dW/dy) N = anisotropy constant, ——//ar r /a \ uv/(dU/dy) £/ref__ _ = reference velocity wVv, 2 _ = kinematic normal stresses —7/v, — ww, — "vw = kinematic shear stresses W^o = surface velocity of rotating cylinder a = flow angle with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::073bd2db606f291545dce1c440fd4e82
https://doi.org/10.2514/3.11813
https://doi.org/10.2514/3.11813
Akademický článek
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