Zobrazeno 1 - 10
of 15
pro vyhledávání: '"Scott L. Goodliff"'
Autor:
Richard L. Campbell, Sally A. Viken, Scott L. Goodliff, Anthony Neal Watkins, Melissa B. Rivers, Michelle N. Lynde, David T. Chan
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cbe371d229c5835f6bc47322e11f47bb
https://doi.org/10.2514/6.2019-2189.c1
https://doi.org/10.2514/6.2019-2189.c1
Autor:
Melissa B. Rivers, Michelle N. Lynde, Richard L. Campbell, Sally A. Viken, David T. Chan, Anthony N. Watkins, Scott L. Goodliff
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f3a8fda8542e370a43154f862847b7d
https://doi.org/10.2514/6.2019-2189
https://doi.org/10.2514/6.2019-2189
Autor:
Melissa B. Rivers, Richard L. Campbell, Anthony Neal Watkins, Michelle N. Lynde, Sally A. Viken, David T. Chan, Scott L. Goodliff
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::370c636245b05d79e5c2a39083997d44
https://doi.org/10.2514/6.2019-2298
https://doi.org/10.2514/6.2019-2298
Autor:
C. Mark Cagle, Scott L. Goodliff, William E. Milholen, Jared S. Fell, Gregory S. Jones, David T. Chan
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
The FAST-MAC circulation control model was modified to test an array of steady and unsteady actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Previous experiments in the FAST-MAC te
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::083d2a1d03dce8fecc14fcc9af023c80
https://doi.org/10.2514/6.2018-1138
https://doi.org/10.2514/6.2018-1138
Autor:
William E. Milholen, David T. Chan, Scott L. Goodliff, LaTunia G. Pack Melton, Gregory S. Jones, Christopher M. Cagle
Publikováno v:
35th AIAA Applied Aerodynamics Conference.
The FAST-MAC circulation control model was modified to test an array of unsteady sweeping-jet actuators at realistic flight Reynolds numbers in the National Transonic Facility at the NASA Langley Research Center. Two types of sweeping jet actuators w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4f46c92f8b0f323caa5ceb32b218cb90
https://doi.org/10.2514/6.2017-3044
https://doi.org/10.2514/6.2017-3044
Publikováno v:
35th AIAA Applied Aerodynamics Conference.
A third wind tunnel test of the FAST-MAC circulation control semi-span model was completed in the National Transonic Facility at the NASA Langley Research Center where the model was configured for transonic testing of the cruise configuration with 0d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::34759ba3e900b9c7320276850e27ae73
https://doi.org/10.2514/6.2017-3246
https://doi.org/10.2514/6.2017-3246
Autor:
Scott L. Goodliff, William E. Milholen, Gregory S. Jones, C. Mark Cagle, Sundareswara Balakrishna, David Butler, David T. Chan
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
The National Transonic Facility is a transonic pressurized cryogenic facility. The development of the high Reynolds number semi-span capability has advanced over the years to include transonic active flow control and powered testing using the sidewal
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13b5c8e0ebdd3dc6a8c2bc1eba456e7c
https://doi.org/10.2514/6.2016-0648
https://doi.org/10.2514/6.2016-0648
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Recent data quality improvements at the National Transonic Facility (NTF) have an intended goal of reducing the Mach number variation in a data point to within unit vector A plus or minus 0.0005, with the ultimate goal of reducing the data repeatabil
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b8d2e8b692bebe5e8793b704a0aa5e2
https://doi.org/10.2514/6.2015-0622
https://doi.org/10.2514/6.2015-0622
Autor:
Joshua A. DeMoss, Gregory S. Jones, Matthew Bailey, Scott L. Goodliff, Sundareswara Balakrishna
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Pressure fluctuations have been measured over the course of several tests in the National Transonic Facility to study unsteady phenomenon both with and without the influence of a model. Broadband spectral analysis will be used to characterize the len
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9d73f00aa6400e5ef3740832e2ea310
https://doi.org/10.2514/6.2015-1557
https://doi.org/10.2514/6.2015-1557
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
A second wind tunnel test of the FAST-MAC circulation control semi-span model was recently completed in the National Transonic Facility at the NASA Langley Research Center. The model allowed independent control of four circulation control plenums pro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0261c5f826813644e0fab64416813f9a
https://doi.org/10.2514/6.2014-2402
https://doi.org/10.2514/6.2014-2402