Zobrazeno 1 - 10
of 11
pro vyhledávání: '"S. D. Heister"'
Autor:
S. D. Heister
Publikováno v:
Proceedings of the 52nd INDUSTRIAL WASTE CONFERENCE May 5–7, 1997
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8db17981d1823210d8560008477ddfbe
https://doi.org/10.1201/9780367813291-66
https://doi.org/10.1201/9780367813291-66
Autor:
S. D. Heister
Publikováno v:
Handbook of Atomization and Sprays ISBN: 9781441972637
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a2c6061e1153d3fea28e68efd0b3c5ab
https://doi.org/10.1007/978-1-4419-7264-4_28
https://doi.org/10.1007/978-1-4419-7264-4_28
Autor:
S. D. Heister
Publikováno v:
Handbook of Atomization and Sprays ISBN: 9781441972637
Plain orifice, or “pressure atomizers” are the most commonly used atomizers due primarily to their simplicity and ease of manufacture. This chapter provides background on the characteristics of these devices in terms of spray production and gener
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b0b7fa4594af13eb9f56abad3b5db5d
https://doi.org/10.1007/978-1-4419-7264-4_27
https://doi.org/10.1007/978-1-4419-7264-4_27
Publikováno v:
Journal of Fluid Mechanics. 220:339-354
A numerical solution for the flow field associated with a compressible pair of counter-rotating vortices is developed. The compressible, two-dimensional potential equation is solved utilizing the numerical method of Osher et al. (1985) for flow regio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3418229f22f84cb1502f680f650e2236
https://doi.org/10.1017/s0022112090003287
https://doi.org/10.1017/s0022112090003287
Autor:
Ann Karagozian, S. D. Heister
Publikováno v:
AIAA Journal. 28:819-827
We describe an analytical/numerical model representing the deflection and mixing of a single gaseous jet in supersonic crossflow. The jet cross section is modeled in terms of a compressible vortex pair that results from viscous and impulsive forces a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2492db0763dd45561aade7bcc7fe60d3
https://doi.org/10.2514/3.25125
https://doi.org/10.2514/3.25125
Publikováno v:
35th Joint Propulsion Conference and Exhibit.
A new class of hypergolic propellants developed by researchers at the Naval Air Warfare Center, China Lake, California, has been examined. These propellants have the properties of being non-toxic and having ideal performance close to that of the trad
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7ac4c5396d88f068a8df58b3b5a7ffd0
https://doi.org/10.2514/6.1999-2878
https://doi.org/10.2514/6.1999-2878
Autor:
S. D. Heister, J. H. Hilbing
Publikováno v:
29th Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7bfa747ee0d03262ae70b615f62b5add
https://doi.org/10.2514/6.1993-2309
https://doi.org/10.2514/6.1993-2309
Publikováno v:
AIAA Journal. 27:1727-1734
Analytical/numerical modeling of the behavior of a single nonreacting liquid jet in compressible (high subsonic and supersonic) crossflows is described here. Inviscid, compressible flow about the elliptical cross-section of the jet is solved numerica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ec828c467f40eadc2d2b42aec4fd7049
https://doi.org/10.2514/3.10327
https://doi.org/10.2514/3.10327
Autor:
S. D. Heister, Ann Karagozian
Publikováno v:
24th Joint Propulsion Conference.
This paper discusses an analytical/numerical model developed to describe the behavior of gaseous jets injected transversely into a subsonic (but compressible) crossflow. The cross section of the jet is modeled as an inviscid, compressible vortex pair
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2238308633ba0d8ed7a989a1bb1cf6c2
https://doi.org/10.2514/6.1988-3270
https://doi.org/10.2514/6.1988-3270
Autor:
S. D. Heister, E. M. Landsbaum
Publikováno v:
21st Joint Propulsion Conference.
Ballistic anomalies, defined as pressure deviations from the normally expected trace, have occurred frequently during solid rocket motor firings. This paper describes techniques for determining the probable cause of such anomalies. Mass and energy ba
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d56d3b1071e939899465c7928d85cbf6
https://doi.org/10.2514/6.1985-1303
https://doi.org/10.2514/6.1985-1303