Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Julius E. Harris"'
Publikováno v:
AIAA Journal. 33:2325-2331
A new two-equation turbulence model based on the exact turbulent kinetic energy and the variance of vorticity or enstrophy equations is developed and used to calculate planar and axisymmetric free shear flows. It is shown that one set of model consta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d31a325169c851528d57b5e20a990f73
https://doi.org/10.2514/3.12987
https://doi.org/10.2514/3.12987
Publikováno v:
AIAA Journal. 33:1391-1397
A transition model for low-speed flows has previously been developed by Young et al. which incorporates first-mode (Tollmien-Schlichting) disturbance information from linear stability theory. The present work extends the model to high-speed flows by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06c35ca0c19c3f0c51860a017569cd60
https://doi.org/10.2514/3.12687
https://doi.org/10.2514/3.12687
Publikováno v:
AIAA Journal. 31:629-636
In spite of many attempts at modelling natural transition, it has not been possible to predict the streamwise intensities. A procedure is developed that incorporates some results of linear stability theory into one-equation and stress model formulati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0cc33a31aae3dc082b3af25925aa0304
https://doi.org/10.2514/3.11596
https://doi.org/10.2514/3.11596
Autor:
Yong-Sun Wie, Julius E. Harris
Publikováno v:
Journal of Aircraft. 28:861-868
Numerical solutions of the three-dimensional, compressible laminar boundary-layer equations for a general aviation fuselage are presented. The numerical procedure is second-order accurate and independent of the cross-flow velocity direction. Numerica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1da0f182af8897cabb9606c186498298
https://doi.org/10.2514/3.46110
https://doi.org/10.2514/3.46110
Autor:
Julius E. Harris, Venkit Iyer
Publikováno v:
Journal of Aircraft. 27:253-261
A fourth-order accurate finite-difference procedure for solving compressible three-dimensional boundarylayer equations is presented and applied to wing and ellipsoid flows. The method is fourth-order accurate normal to the surface and second-order ac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82b05d8dc5b67d0ac9117914011dc660
https://doi.org/10.2514/3.45927
https://doi.org/10.2514/3.45927
Autor:
Dana J. Morris, Julius E. Harris
Publikováno v:
Proceedings of the Fourth International Conference on Numerical Methods in Fluid Dynamics ISBN: 3540071393
A technique for solving three-dimensional boundary-layer flows is presented. The governing equations are transformed to obtain a nondimensional form and a similarity-type transform is defined for the normal coordinate and velocity. The resulting equa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2dc9f9d1f8f94a190f438a28f552de5
https://doi.org/10.1007/bfb0019752
https://doi.org/10.1007/bfb0019752
Publikováno v:
33rd Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3fba6e7d97debb980218ab9d2fe6349f
https://doi.org/10.2514/6.1995-360
https://doi.org/10.2514/6.1995-360
Publikováno v:
12th Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a717469be536acf19ecfe45d1119ded8
https://doi.org/10.2514/6.1994-1851
https://doi.org/10.2514/6.1994-1851
Publikováno v:
10th Applied Aerodynamics Conference.
In spite of many attempts at modeling natural transition, it has not been possible to predict the streamwise intensities. A procedure is developed which incorporates some results of linear stability theory into one-equation and stress model formulati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::83fa51ced44c298f397f53f54d4ae419
https://doi.org/10.2514/6.1992-2669
https://doi.org/10.2514/6.1992-2669
Autor:
Venkit Iyer, Julius E. Harris
Publikováno v:
27th Aerospace Sciences Meeting.
Laminar flow control and drag reduction research requires accurate boundary layer solutions as input to the three-dimensional stability analysis procedures currently under development. In support of these major programs, a fourth-order accurate finit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df6e3518a6c33352e4e8946f2e244912
https://doi.org/10.2514/6.1989-130
https://doi.org/10.2514/6.1989-130