Zobrazeno 1 - 10
of 18
pro vyhledávání: '"S. Naomi McMillin"'
Autor:
Daniel Maldonado, Craig A. Hunter, Sally A. Viken, Jared C. Duensing, S. Naomi McMillin, Neal T. Frink, Jeffrey A. Housman, James C. Jensen, Cetin C. Kiris
Publikováno v:
AIAA Scitech 2020 Forum.
A joint effort between the NASA Ames and Langley Research Centers was undertaken to analyze the Mach 0.745 variant of the Boeing Transonic Truss-Braced Wing (TTBW) Design. Two different flow solvers, LAVA and USM3D, were used to predict the TTBW flig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b03f5fd2672e3499889a4f211aa27f96
https://doi.org/10.2514/6.2020-1649
https://doi.org/10.2514/6.2020-1649
Autor:
Jamie G. Meeroff, Patrick R. Shea, Henry C. Lee, Nettie Roozeboom, Stuart E. Rogers, Derek J. Dalle, S. Naomi McMillin
Publikováno v:
AIAA Aviation 2019 Forum.
A comparison of surface pressure coefficient measurements obtained using pressure-sensitive paint (PSP) measurements with predictions from the computational fluid dynamics (CFD) code FUN3D is presented for the NASA SLS Block 1B crew vehicle. Overall,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::57b0ba4d87c52d5455151cb3a5fd2b63
https://doi.org/10.2514/6.2019-3301
https://doi.org/10.2514/6.2019-3301
Publikováno v:
AIAA Scitech 2019 Forum.
Models including nonlinear and unsteady behaviors are developed for the longitudinal axis of the NASA Generic T-Tail Aircraft over a large range of angle of attack. These models are based on computational simulations of forced-oscillation tests in a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2435e273837822ff85764f4429ad89e9
https://doi.org/10.2514/6.2019-0819
https://doi.org/10.2514/6.2019-0819
Autor:
Matthew R. Sexton, Daniel Tompkins, Karen A. Deere, S. Naomi McMillin, Melissa Carter, Michael J. Schuh, Paul M. Stremel
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::937eb99a8c9a1659a35efc34022ab5f2
https://doi.org/10.2514/6.2016-0264
https://doi.org/10.2514/6.2016-0264
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
A computational study was performed for a Hybrid Wing Body configuration that was focused at transonic cruise performance conditions. In the absence of experimental data, two fully independent computational fluid dynamics analyses were conducted to a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3d684431be16f84f191245bf77158c6a
https://doi.org/10.2514/6.2016-0266
https://doi.org/10.2514/6.2016-0266
Publikováno v:
Journal of Aircraft. 42:586-599
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall. The technical approach employed focused on correlating
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::91793ea644ce9f5ba6a2db8df802537f
https://doi.org/10.2514/1.3152
https://doi.org/10.2514/1.3152
Publikováno v:
Journal of Aircraft. 41:464-473
An approach is provided to answer the question of whether one can rely solely on static data taken during a transonic model test to provide the certainty needed that a new aircraft will or will not have abrupt wing stall (AWS) events during its fligh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d3d0f106156c64030199b9ce34134b5d
https://doi.org/10.2514/1.2770
https://doi.org/10.2514/1.2770
Publikováno v:
Journal of Aircraft. 41:448-455
Ar eview of the experimental program for four different aircraft configurations conducted as part of the Abrupt Wing Stall Program has been made. Several candidate figures of merit from conventional static-tunnel tests are summarized and correlated w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1b0ca7318f1a2605900c872351b1d2b
https://doi.org/10.2514/1.2768
https://doi.org/10.2514/1.2768
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall. The technical approach employed focused on correlating
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4577e639b28718093fbd6129b92a96d3
https://doi.org/10.2514/6.2003-591
https://doi.org/10.2514/6.2003-591
Publikováno v:
Flight Simulation Technologies Conference and Exhibit.
A computational study on a 65-deg delta wing at a freestream Mach number of 1.60 has been conducted by obtaining conical Reynolds-averaged Navier-Stokes solutions on a parametric series of geometries which varied in leading-edge radius and/or circula
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::af0eb4f2805a313cf3aa2c6bdb077138
https://doi.org/10.2514/6.1990-3029
https://doi.org/10.2514/6.1990-3029