Zobrazeno 1 - 10
of 34
pro vyhledávání: '"JOSEPH, Olejniczak"'
Publikováno v:
2019年度衝撃波シンポジウム 講演論文集 = Proceedings of the Symposium on Shock Waves in Japan, FY2019.
2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県
Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan
Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::c7b8b6dd8bc0db205d4af0436bb9b989
http://id.nii.ac.jp/1696/00046705/
http://id.nii.ac.jp/1696/00046705/
Publikováno v:
Journal of Thermophysics and Heat Transfer. 29:858-862
資料番号: AC1500103000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4eb477b9e7e28400cbf803d6273cf5ba
https://doi.org/10.2514/1.t4478
https://doi.org/10.2514/1.t4478
Autor:
Joseph Olejniczak, Randolph P. Lillard
Publikováno v:
2017 IEEE Aerospace Conference.
This paper presents the results of a NASA initiated Agency-wide assessment to better characterize the risks and potential mitigation approaches associated with landing human class payloads on Mars. Due to the criticality and long-lead nature of advan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bbe28969b8cf0c5378ba2670efe5bb11
https://doi.org/10.1109/aero.2017.7943587
https://doi.org/10.1109/aero.2017.7943587
Autor:
Brett A. Cruden, Aaron M. Brandis, Jay H. Grinstead, Joseph Olejniczak, Lindsay Kirk, Randolph P. Lillard, Hideyuki Tanno, Tomoyuki Komuro
Publikováno v:
45th AIAA Thermophysics Conference.
Radiance measurements in air at enthalpies from 8-20 MJkg have been made over a 250mm diameter flat-faced test article in Japan Aerospace Exploration Agency's HIgh-Enthalpy Shock Tunnel (HIEST). Measurements were made in the ultraviolet region (200-4
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21e751872ca39c8bf96d58f0007edee5
https://doi.org/10.2514/6.2015-2512
https://doi.org/10.2514/6.2015-2512
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Computational assessments were performed to size boundary layer trips for a scaled Apollo capsule model in the High Enthalpy Shock Tunnel (HIEST) facility at the JAXA Kakuda Space Center in Japan. For stagnation conditions between 2 MJ/kg and 20 MJ/k
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::71f6dd1b7e1442e23aa05f018ad75c3a
https://doi.org/10.2514/6.2015-0209
https://doi.org/10.2514/6.2015-0209
Autor:
Imelda Terrazas-Salinas, David M. Driver, Takeharu Sakai, Joseph Olejniczak, Chul B. Park, T. Mark Hightower, George A. Raiche
Publikováno v:
Journal of Thermophysics and Heat Transfer. 20:672-679
Four experimental methods of determining the enthalpy of the flow in an arc-jet facility that is, the heat balance method, the sonic throat method, the heat transfer method, and the emission-spectroscopic method, are compared with a computational flu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::41938490ec13e4e499420ef32c1724d7
https://doi.org/10.2514/1.15744
https://doi.org/10.2514/1.15744
Autor:
Hideyuki Tanno, Tomoyuki Komuro, Kazuo Sato, Katsuhiro Itoh, Randolph P. Lillard, Joseph Olejniczak, Jay H. Grinstead
Publikováno v:
52nd Aerospace Sciences Meeting.
An aeroheating measurement test campaign of an Apollo capsule model with laminar and turbulent boundary layer was performed in the free-piston shock tunnel HIEST at JAXA Kakuda Space Center. A 250mm-diameter 6.4%-scaled Apollo CM capsule model made o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c65cc5e6246518d2c0a6e7104822e38e
https://doi.org/10.2514/6.2014-0434
https://doi.org/10.2514/6.2014-0434
Autor:
Graham V. Candler, Michael J. Wright, Krishnendu Sinha, Joseph Olejniczak, Alexander Smits, T. D. Magruder
Publikováno v:
AIAA Journal. 38:2268-2276
A series of experiments was conducted in the Princeton University Mach 8 Wind Tunnel to study shock interactions on axisymmetric double-cone geometries. Schlieren images and surface-pressure data were taken. Two models were tested, which were expecte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c5a0e186ce8e8560beaabf5605231741
https://doi.org/10.2514/2.918
https://doi.org/10.2514/2.918
Autor:
P. J. Gage, Dinesh K. Prabhu, Periklis Papadopoulos, Joseph Olejniczak, Dave Olynick, Michael J. Wright
Publikováno v:
Advances in Engineering Software. 31:697-705
Web browser interfaces have been developed for geometry generation, volume grid generation, Computational fluid dynamics (CFD) solver execution and solution inspection. These interfaces access only a subset of the software's capability because they a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc9cffd8c14bbd427810ce4d0bc12e7b
https://doi.org/10.1016/s0965-9978(00)00028-4
https://doi.org/10.1016/s0965-9978(00)00028-4
Publikováno v:
Journal of Thermophysics and Heat Transfer. 13:431-440
A series of experiments designed to study reacting nitrogen flow over double-wedge geometries was conducted in the T5 shock tunnel at the California Institute of Technology. These experiments were designed using computational fluid dynamics to test n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b87c55bd1dde816be569c84990d3dfa5
https://doi.org/10.2514/2.6481
https://doi.org/10.2514/2.6481