Zobrazeno 1 - 10
of 33
pro vyhledávání: '"Bernhard H. Anderson"'
Autor:
Bernhard H. Anderson, Harold S. Haller
Publikováno v:
Quality Engineering. 23:46-58
This article offers an approach to reducing time and cost of experimentation in large wind tunnels by combining computer simulations of fluid dynamics test models with small sets of experimental data. To demonstrate the viability of this technique, t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::118c4f9b705748bdd4b8a12146df7332
https://doi.org/10.1080/08982112.2010.505221
https://doi.org/10.1080/08982112.2010.505221
Autor:
Bernhard H. Anderson
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
This paper presents a statistical methodology whereby the probability limits associated with CFD grid resolution of inlet flow analysis can be determined which provide quantitative information on the distribution of that error over the specified oper
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::99c7c60a0497d7b2d00abd269d12f4cf
https://doi.org/10.2514/6.2014-3801
https://doi.org/10.2514/6.2014-3801
Autor:
Bernhard H. Anderson, Lois Weir
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Supersonic inlets with external compression, having a good level performance at the critical operating point, exhibit a marked instability of the flow in some subcritical operation below a critical value of the capture mass flow ratio. This takes the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca34f810230382ecc997bf4c3bf5d0df
https://doi.org/10.2514/6.2014-3799
https://doi.org/10.2514/6.2014-3799
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Development of commercial supersonic aircraft has been hindered by many related factors including fuel-efficiency, economics, and sonic-boom signatures that have prevented over-land flight. Materials, propulsion, and flight control technologies have
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::912f08f3abbdd1395ffc294b7723f8ae
https://doi.org/10.2514/6.2014-3802
https://doi.org/10.2514/6.2014-3802
Autor:
Bernhard H. Anderson, James Gibb
Publikováno v:
Journal of Aircraft. 35:513-520
The theoretical and experimental work carried out under the NASA/MOD joint aeronautical program has shown that computational fluid dynamics (CFD) vortex-generator installation designs successfully managed inlet-duct now distortion and that significan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6c34c1681b4dd9dd6d0d80e0261c0de2
https://doi.org/10.2514/2.2340
https://doi.org/10.2514/2.2340
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Hybrid flow control, a combination of micro-ramps and micro-jets, was experimentally investigated in the 15x15 cm Supersonic Wind Tunnel (SWT) at the NASA Glenn Research Center. Full factorial, a design of experiments (DOE) method, was used to develo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f25eb6b481d6087a9fa14c380da1254
https://doi.org/10.2514/6.2012-48
https://doi.org/10.2514/6.2012-48
Publikováno v:
Journal of Propulsion and Power. 10:661-667
A three-dimensional implicit full Navier-Stokes (FNS) analysis and a three-dimensional reduced Navier-Stokes (RNS) initial value space marching solution technique have been applied to a class of separated flow problems within a diffusing S-duct confi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::792547013690b9b46f45853c50315384
https://doi.org/10.2514/3.23777
https://doi.org/10.2514/3.23777
Publikováno v:
41st AIAA Fluid Dynamics Conference and Exhibit.
A passive method of controlling normal shock/boundary layer interactions (SBLIs) for external compression inlet applications is the use of micro-ramps for boundary layer control (BLC). These devices were placed upstream of normal SBLIs of various sho
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::468816eadcef211d069c1f920f0d1874
https://doi.org/10.2514/6.2011-3911
https://doi.org/10.2514/6.2011-3911
Autor:
Bernhard H. Anderson, James Gibb
Publikováno v:
Journal of Propulsion and Power. 9:422-430
The present study demonstrates that the reduced Navier-Stokes RNS3D code can be used very effectively to develop a vortex generator installation to minimize the engine face circumferential distortion by controlling secondary flow. The computing times
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fce5c4554a0de9da416dfcfa73a81409
https://doi.org/10.2514/3.23638
https://doi.org/10.2514/3.23638
Publikováno v:
Journal of Propulsion and Power. 8:1266-1272
The present study demonstrates that the reduced Navier-Stokes code (RNS3D) can be used very effectively to develop a vortex generator installation for the purpose of minimizing the engine-face circumferential distortion by controlling the development
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c6a75a91ce1781d1377164aa5b8e873
https://doi.org/10.2514/3.11472
https://doi.org/10.2514/3.11472