Zobrazeno 1 - 10
of 13
pro vyhledávání: '"H. L. Seegmiller"'
Autor:
Michael E. Olsen, H. L. Seegmiller
Publikováno v:
AIAA Journal. 31:1744-1752
An experiment was performed on a low-aspect ratio wing to define the limits of the validity of codes which are used to predict the flow over modern fighter configurations. The focus of the experiment is to provide data at or near the true operating c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::80f008c6b91e6f88f32e066293e66f8f
https://doi.org/10.2514/3.49105
https://doi.org/10.2514/3.49105
Publikováno v:
21st Fluid Dynamics, Plasma Dynamics and Lasers Conference.
In this paper experimental measurements are compared with Navier-Stokes calculations using seven different turbulence models for the internal flow in a two-dimensional U-duct. The configuration is representative of many internal flows of engineering
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd74837f0cebc79aeeb9910875a3aaca
https://doi.org/10.2514/6.1990-1484
https://doi.org/10.2514/6.1990-1484
Publikováno v:
AIAA Journal. 16:1262-1270
An investigation of the transonic flow over a circular arc airfoil was conducted to obtain basic information for turbulence modeling of shock-induced separated flows and to verify numerical computer codes which are being developed to simulate such fl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4d61b14352539ff543a42ee6c9fa83ad
https://doi.org/10.2514/3.61042
https://doi.org/10.2514/3.61042
Publikováno v:
AIAA Journal. 18:1059-1065
An investigation of trailing-edge flows at high Reynolds number and subsonic Mach numbers is presented. Symmetric and asymmetric trailing-edge flows are studied, each flow having pressure gradient regions upstream of the trailing edge similar to an a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::152ae811793edf2d5aea30f31ddabd39
https://doi.org/10.2514/3.50854
https://doi.org/10.2514/3.50854
Autor:
H. L. Seegmiller, David M. Driver
Publikováno v:
AIAA Journal. 23:163-171
Experimental data have been obtained in an incompressible turbulent flow over a rearward-facing step in a diverging channel flow. Mean velocities, Reynolds stresses, and triple products that were measured by a laser Doppler velocimeter are presented
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a9099f8758a4e81cdd94157002f6d04
https://doi.org/10.2514/3.8890
https://doi.org/10.2514/3.8890
Publikováno v:
AIAA Journal. 18:489-496
Conditionally sampled, ensemble-averaged velocity measurements, made with a laser velocimeter, were taken in the flowfield over the rear half of an 18% thick circular arc airfoil at zero incidence tested at M = 0.76 and at a Reynolds number based on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e33f2fc521a40de238b37a3e2125d9b
https://doi.org/10.2514/3.50782
https://doi.org/10.2514/3.50782
Autor:
C. E. Derose, H. L. Seegmiller, Joseph G. Marvin, William K. Lockman, George G. Mateer, C. C. Pappas
Publikováno v:
Journal of Spacecraft and Rockets. 9:573-579
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::222c595b357a505c33b44460eb7cf7c4
https://doi.org/10.2514/3.61748
https://doi.org/10.2514/3.61748
Publikováno v:
16th Fluid and Plasmadynamics Conference.
A detailed investigation of the unsteadiness in a reattaching, turbulent shear layer is reported. Laser-Doppler velocimeter measurements were conditionally sampled on the basis of instantaneous flow direction near reattachment. Conditions of abnormal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b178a1c760bcbe6b4fceb33e013da54c
https://doi.org/10.2514/6.1983-1712
https://doi.org/10.2514/6.1983-1712
Autor:
H. L. Seegmiller, D. M. Driver
Publikováno v:
3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference.
Experimental data have been obtained in an incompressible turbulent flow over a rearward-facing step with superimposed adverse pressure gradient. Mean velocities, Reynolds stresses and triple-products measured by a laser Doppler velocimeter are prese
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::325087c9d5e89a59e4dd0bf72d3d47fc
https://doi.org/10.2514/6.1982-1029
https://doi.org/10.2514/6.1982-1029
Publikováno v:
19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d6472cb32c61d638c91d71240dc50ac9
https://doi.org/10.2514/6.1987-1241
https://doi.org/10.2514/6.1987-1241