Zobrazeno 1 - 10
of 110
pro vyhledávání: '"Paul I. King"'
Publikováno v:
Journal of Propulsion and Power. 33:1448-1458
A premixed supply of fuel and oxidizer was fed through five concentric feed slots and detonated in a rotating detonation engine, representing the first known successful airbreathing premixed rotati...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1098d16563b04931bce5e194dd1104ec
https://doi.org/10.2514/1.b36261
https://doi.org/10.2514/1.b36261
Publikováno v:
Journal of Propulsion and Power. 33:1063-1073
Rotating detonation engines offer the promise of pressure gain combustion in aeronautical combustors where (normally) stagnation pressure decreases. For practical reasons, current experimental rotating detonation engine designs include separate strea
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::14ef429e2403070c1f1687b97bbf20c4
https://doi.org/10.2514/1.b36259
https://doi.org/10.2514/1.b36259
Publikováno v:
Journal of Propulsion and Power. 30:1528-1536
Theoretically, pressure-gain combustion like that of a pulsed-detonation combustor allows heat addition with reduced entropy loss compared to a typical steady deflagration combustor. The pulsed-detonation combustor is inherently unsteady, and time-re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7741aec86bad104823f0060c5f1a63b2
https://doi.org/10.2514/1.b34966
https://doi.org/10.2514/1.b34966
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
A premixed supply of fuel and oxidizer was successfully fed through five concentric feed slots and detonated in a rotating detonation engine (RDE). This study reports the first known successful air-breathing premixed RDE. The premixed flow maintained
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1eb54a80244f9674cbbde8465eb1f0e7
https://doi.org/10.2514/6.2016-1404
https://doi.org/10.2514/6.2016-1404
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::212b44874158a8abe920053e6f67848a
https://doi.org/10.2514/6.2016-0127
https://doi.org/10.2514/6.2016-0127
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Detonation cell sizes of fuel and oxidizer combinations are the fundamental length scale of detonations. The cell size is correlated to the dynamic detonation properties. One of the properties, detonability, is the motivation for this research in ord
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44bfbe915a1507d8ba148543ed45d351
https://doi.org/10.2514/6.2016-0442
https://doi.org/10.2514/6.2016-0442
Publikováno v:
Journal of Propulsion and Power. 25:571-582
This study explores the effect of adding a pylon to the leading edge of a cavity flameholder in a scramjet combustor. Data were obtained through a combination of wind-tunnel experimentation and steady-state computational fluid dynamics. Wind-tunnel d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bfd28ab9f868713cd62ea59f10dda1ef
https://doi.org/10.2514/1.39546
https://doi.org/10.2514/1.39546
Publikováno v:
Journal of Propulsion and Power. 24:788-796
Practical operation of pulsed detonation propulsion requires operation on kerosene-based jet fuels. These low vapor pressure fuels remain in liquid form at typical pulsed detonation inlet conditions and residence times, and the subsequent presence of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6872df4581fb61945c674b2fcab913c5
https://doi.org/10.2514/1.28412
https://doi.org/10.2514/1.28412
Publikováno v:
Journal of Propulsion and Power. 24:403-409
Complete knowledge of the heat transfer over the surfaces of turbine components within their harsh operating environments is key to knowing the durability of a given airfoil design. Here, a nominal turbine inlet vane was tested for unsteady-heat-load
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdb4d760345fe16a04ca8f7225cfaf01
https://doi.org/10.2514/1.28501
https://doi.org/10.2514/1.28501
Publikováno v:
Journal of Propulsion and Power. 24:395-402
Historically, there has been a distinct difference between the design of turbomachinery airfoils for aerodynamic performance and that for durability. However, future aeroengine systems will require ever-increasing levels of turbine inlettemperature,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::030bb7d0bac3e017e1659e81576e63d9
https://doi.org/10.2514/1.28530
https://doi.org/10.2514/1.28530