Zobrazeno 1 - 10
of 10
pro vyhledávání: '"B. G. McLachlan"'
Autor:
J. A. Schreiner, J. M. Strong, B. G. McLachlan, Robert A. Kennelly, James H. Bell, Martin Gouterman, H. Park, Jean Gallery, Stephen C. Smith
Publikováno v:
Journal of Aircraft. 32:217-227
The pressure-sensitive paint method was used in the test of a high-sweep oblique wing model, conducted in the NASA Ames 9- by 7-ft Supersonic Wind Tunnel. Surface pressure data was acquired from both the luminescent paint and conventional pressure ta
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1aedbfa19cd2e9d2bcc84dfa68b98482
https://doi.org/10.2514/3.56921
https://doi.org/10.2514/3.56921
Autor:
B. G. Mclachlan
Publikováno v:
Journal of Aircraft. 26:817-821
An experimental study of the flow past a two-dimensional circulation control airfoil under steady leading/trailing edge blowing was conducted. The effect of varying jet momentum on the flow field was determined through the use of flow visualization a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca5902601145a0d2a90d42573006eb81
https://doi.org/10.2514/3.45846
https://doi.org/10.2514/3.45846
Publikováno v:
10th Atmospheric Flight Mechanics Conference.
The flow field generated by a two-dimensional airfoil with a statically deflected flap type spoiler has been experimentally studied. Subsonic tests ascertained the effect of varying spoiler deflection and angle of attack on the flow field at two Reyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b39380ed1b7be8582455e255d21b2a4f
https://doi.org/10.2514/6.1983-2131
https://doi.org/10.2514/6.1983-2131
Publikováno v:
1st National Fluid Dynamics Conference.
This paper describes progress in validating incompressible Navier-Stokes codes using image-processed flow-field data. Solutions of the Navier-Stokes equations using a predictor/corrector scheme are compared directly with experimental data. A uniform
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b6b646bf2e9c8593044009b250fe8265
https://doi.org/10.2514/6.1988-3521
https://doi.org/10.2514/6.1988-3521
Publikováno v:
22nd Aerospace Sciences Meeting.
Preliminary results of an experimental study of the flow field structure within a rectangular jet ejector are presented. The tests determined the effect of primary jet heating and ejector duct width on the flow field at a fixed jet exit Mach number o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea6cdc51843f505c1aedf8d874f37852
https://doi.org/10.2514/6.1984-571
https://doi.org/10.2514/6.1984-571
Autor:
A. Ayoub, B. G. Mclachlan
Publikováno v:
19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference.
The flow past a delta wing of aspect ratio one is examined at angles of attack ranging from 25 deg to 90 deg. On the basis of detailed observations of the flow in a water channel, using laser-induced fluorescence, four angle of attack flow regimes ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40d86b272806a2c6a3c2ed77fd7b02a2
https://doi.org/10.2514/6.1987-1230
https://doi.org/10.2514/6.1987-1230
Autor:
B. G. Mclachlan, A. Krothapalli
Publikováno v:
17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference.
Results of an experimental study of the flow structure of a subsonic jet issuing from an array of rectangular lobes, equally spaced with their small dimensions in a line, are presented. The tests determined the affect of jet exit Mach number variatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b739f16697c768ac44b13cf7faa5e881
https://doi.org/10.2514/6.1984-1656
https://doi.org/10.2514/6.1984-1656
Autor:
B. G. Mclachlan
Publikováno v:
25th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6f4b2efb94a58c3590ad7a050bf31cf
https://doi.org/10.2514/6.1987-157
https://doi.org/10.2514/6.1987-157
Autor:
Y.-C. Cho, B. G. Mclachlan
Publikováno v:
SPIE Proceedings.
A PC based image processing system was employed to determine the instantaneous velocity field of a two-dimensional unsteady flow. The flow was visualized using a suspension of seeding particles in water, and a laser sheet for illumination. With a fin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06632ae3598c1704bc8f876abfee77dd
https://doi.org/10.1117/12.942134
https://doi.org/10.1117/12.942134
Autor:
B. G. McLachlan, A. Ayoub
Publikováno v:
Physics of Fluids. 31:2391-2391
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b003c62783d27abba102f4728a8f615a
https://doi.org/10.1063/1.4738826
https://doi.org/10.1063/1.4738826