Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Dasheng Lim"'
Publikováno v:
Journal of Spacecraft and Rockets. 58:1444-1452
An experimental test campaign was conducted for a rotating detonation rocket engine (RDRE) using gaseous oxygen and RP-2 at operating pressures of 3–18 atm. The copper chamber outer wall was instru...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::14d5d005fbdc62650cf3fdded2365782
https://doi.org/10.2514/1.a34840
https://doi.org/10.2514/1.a34840
Publikováno v:
Shock Waves. 31:717-726
Angled and tapered injectors have been subjected to detonation fronts at high-pressure conditions and analyzed using high-speed videos. A total of 846 tests were conducted to characterize refill times and back-flow distances of nine different injecto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8adcc81a09b15b6528754650c589af7
https://doi.org/10.1007/s00193-021-01010-0
https://doi.org/10.1007/s00193-021-01010-0
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ef878fb513d10633b1cb03f6d520d2ef
https://doi.org/10.2514/6.2020-0195.c1
https://doi.org/10.2514/6.2020-0195.c1
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b92761169d765fae97563a8e4f17766
https://doi.org/10.2514/6.2020-0195
https://doi.org/10.2514/6.2020-0195
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e45d2d8ff6687d6502482d9fd0173d49
https://doi.org/10.2514/6.2019-1513
https://doi.org/10.2514/6.2019-1513
Autor:
Dasheng Lim
The results of two experimental studies are presented in this document. The first was an investigation on the transient response of plain orifice liquid injectors to transverse detonation waves at elevated pressures of 414, 690, and 1,030 kPa (60, 10
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9593ff08453e45157808a14254772f80
Publikováno v:
Journal of Spacecraft & Rockets. Sep2021, Vol. 58 Issue 5, p1444-1452. 9p.
Transient Response of a Liquid Injector to a Transverse Detonation Wave at Elevated Initial Pressure
Autor:
Dasheng Lim, Stephen D. Heister
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff63b761ff93cbf35684d077152b8a12
https://doi.org/10.2514/6.2018-0632
https://doi.org/10.2514/6.2018-0632
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6bbd496cdbd879254d6d316f1e4ed12b
https://doi.org/10.2514/6.2016-4979
https://doi.org/10.2514/6.2016-4979
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
A series of experiments has been performed to study the transient response of a liquid injector to a transverse detonation wave. Using an optically accessible test article and a high speed camera, images were captured at 80,000 frames per second to r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a19d2e8ab076b2c2b8a37bbcf1eca7b0
https://doi.org/10.2514/6.2015-3767
https://doi.org/10.2514/6.2015-3767