Zobrazeno 1 - 10
of 30
pro vyhledávání: '"Lisa W. Griffin"'
Autor:
Jeffrey West, Peter Liever, Andrew Weaver, Thomas P. Shurtz, Manuel Gale, William C. Krolick, Lisa W. Griffin
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7f8b071b55c9150e358798971c83addd
https://doi.org/10.2514/6.2022-2319
https://doi.org/10.2514/6.2022-2319
Publikováno v:
Journal of Propulsion and Power. 20:486-491
The turbines used in rocket-engine applications are often partial-admission turbines, meaning that the flow enters the rotor over only a portion of the annulus. These turbines have been traditionally analyzed, however, assuming full-admission charact
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64f235722f1610d4a980a5b44f4ec3fe
https://doi.org/10.2514/1.10379
https://doi.org/10.2514/1.10379
Publikováno v:
Journal of Propulsion and Power. 18:1305-1308
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cfb1b61dd7fe0a7028975abe9518578
https://doi.org/10.2514/2.6068
https://doi.org/10.2514/2.6068
Publikováno v:
Journal of Propulsion and Power. 18:509-518
There is growing interest to adopt supersonic turbines for rocket propulsion. However, this technology has not been actively investigated in the United States for the last three decades. To aid design improvement, a global optimization framework comb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9fb3741a9aac4a7437fa80c41921f46e
https://doi.org/10.2514/2.5991
https://doi.org/10.2514/2.5991
Publikováno v:
Journal of Turbomachinery. 118:636-642
An experimental/analytical study has been conducted to determine the performance improvements achievable by circumferentially indexing succeeding rows of turbine stator airfoils. A series of tests was conducted to experimentally investigate stator wa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e8729209c31177e7479ee5ab9a24f62
https://doi.org/10.1115/1.2840919
https://doi.org/10.1115/1.2840919
Autor:
Lisa W. Griffin, Daniel J. Dorney, Yolanda Mack, Raphael T. Haftka, Frank W. Huber, Lauren Mahorter Snellgrove, Wei Shyy
Publikováno v:
Hong Kong University of Science and Technology
†† ‡‡ , A response surface-based dual-objective design optimization was conducted in the preliminary design of a compact radial turbine for an expander cycle rocket engine. The optimization objective was to increase the efficiency of the turb
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bc3f6fbf64a5987b2e72f917a9f8f8e7
https://doi.org/10.2514/6.2006-5046
https://doi.org/10.2514/6.2006-5046
Publikováno v:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
An extensive computational effort has been performed in order to investigate the nature of unsteady flow in the fuel line supplying the three Space Shuttle Main Engines during flight. Evidence of high cycle fatigue (HCF) in the flow liner one diamete
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4ae6bfe0e421b8bef9a317d4e675c93a
https://doi.org/10.2514/6.2006-5073
https://doi.org/10.2514/6.2006-5073
Autor:
Jeffry Rothermel, Frank W. Huber, Stephen Skelley, Lisa W. Griffin, Daniel J. Dorney, Randall J. Thornton, John C. Forbes
Publikováno v:
Volume 1: Symposia, Parts A and B.
As part of the development of technologies for rocket engines that will power spacecraft to the Moon and Mars, a program was initiated to develop a conceptual upper stage engine with wide flow range capability. The resulting expander cycle engine des
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98a89a2bcb801ffe7c40cc65f5b6c77e
https://doi.org/10.1115/fedsm2006-98101
https://doi.org/10.1115/fedsm2006-98101
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
In order to mitigate the risk of rocket engine development, accurate analysis of turbomachiner y components is required. As part of a program at NASA/Marshall Space Flight Center to improve analytical tools, a two -stage supersonic turbine was recent
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8ba276ea5974f310a1f141d543fcc199
https://doi.org/10.2514/6.2003-5071
https://doi.org/10.2514/6.2003-5071
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Understanding the unsteady aspects of rotor flow fields is critical to the successful design of rocket engine turbines. A technology program is currently being conducted at NASA's Marshall Space Flight Center to increase the understanding of unsteady
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f438f56fc56bccce25781f7f875b6c4d
https://doi.org/10.2514/6.2003-4916
https://doi.org/10.2514/6.2003-4916