Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Michael Rybalko"'
Publikováno v:
Journal of Propulsion and Power. 32:360-372
The data collected in the 8×6 ft supersonic wind tunnel at the NASA John H. Glenn Research Center of a low-boom supersonic inlet have been analyzed and compared to computational results generated using a detached eddy simulation methodology based on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e30157172a914980255fc9c2242014ad
https://doi.org/10.2514/1.b35603
https://doi.org/10.2514/1.b35603
Autor:
Michael Rybalko, Eric Loth
Publikováno v:
AIAA Journal. 53:3700-3711
The application of subsonic and supersonic vortex generators for flow control in an external compression, axisymmetric low-boom concept inlet was investigated experimentally and computationally. The low-boom inlet design is conceptually based on a pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1cc8d497f30457d2b9ddef20934b9109
https://doi.org/10.2514/1.j054050
https://doi.org/10.2514/1.j054050
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Spectral analysis of a low-boom axisymmetric external compression inlet has been performed using Schlieren video and experimental unsteady surface pressure readings as a function of mass flow rates. The experimental data was obtained for fixed inlet
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ef67468b40930b8fbac7b0feb07e15c
https://doi.org/10.2514/6.2016-0532
https://doi.org/10.2514/6.2016-0532
Publikováno v:
Powder Technology. 221:105-113
A continuous random walk (CRW) turbulent diffusion model was adapted for Lagrangian particles within gas flowfields simulated by hybrid RANS/LES methodologies. The methodology was designed to model all the particle diffusion in RANS regions and model
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::db5a309ceeb60afb72711a8f6c9940c1
https://doi.org/10.1016/j.powtec.2011.12.042
https://doi.org/10.1016/j.powtec.2011.12.042
Publikováno v:
Journal of Propulsion and Power. 28:71-82
T HE interaction of a shock wavewith a turbulent boundary layer constitutes a fundamental problem of high-speed fluid mechanics. A detailed survey of past work on high-speed interactions has been carried out by Settles and Dolling [1] and Smits and D
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3ee14b582deddb50ac48633ab20f3b90
https://doi.org/10.2514/1.b34241
https://doi.org/10.2514/1.b34241
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A low-boom supersonic inlet was investigated in terms of stagnation pressure distribution as well as pressure and shock dynamics at near design conditions. The low-boom inlet design considered in this work is based on previous scale model 1’x1’ w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3d51d25cae11c961d140f2c0adbd421
https://doi.org/10.2514/6.2013-15
https://doi.org/10.2514/6.2013-15
Autor:
Michael Rybalko, Eric Loth
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::026d45cf48f7dc35106f0c91338b3eeb
https://doi.org/10.2514/6.2012-15
https://doi.org/10.2514/6.2012-15
Autor:
Michael Rybalko, Eric Loth
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2be7c1b209dc9488e0ce2bd21e8f25d
https://doi.org/10.2514/6.2011-3803
https://doi.org/10.2514/6.2011-3803
Publikováno v:
5th Flow Control Conference.
The effects of flow control devices for an axisymmetric external compression supersonic inlet are investigated. Specifically, vortex generators (VGs) are placed in the subsonic diffuser to decrease radial distortion at the diffuser exit. The performa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bad1fc3ae7994cf16d400cd55c0ccf5b
https://doi.org/10.2514/6.2010-4253
https://doi.org/10.2514/6.2010-4253
Publikováno v:
39th AIAA Fluid Dynamics Conference.
The application of vortex generators for flow control in an external compression, axisymmetric, low-boom concept inlet was investigated using RANS simulations with three-dimensional (3-D), structured, chimera (overset) grids and the WIND-US code. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b76ca79defb492c0a805051effe9cb04
https://doi.org/10.2514/6.2009-4206
https://doi.org/10.2514/6.2009-4206