Zobrazeno 1 - 10
of 10
pro vyhledávání: '"David P. Stechmann"'
Publikováno v:
Journal of Spacecraft and Rockets. 56:887-898
A simplified theoretical treatment of rotating detonation engine (RDE) performance is developed for rocket applications with traceability to current combustion technology. In particular, the influe...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d07269074d0e0bd0d9b4fd42db79bc42
https://doi.org/10.2514/1.a34313
https://doi.org/10.2514/1.a34313
Publikováno v:
Journal of Propulsion and Power. 35:125-140
Rotating detonation engines (RDEs) represent a promising technology for improving the performance of existing aerospace combustors, but additional research is needed to characterize the operability...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f63e4b6c2bba76090dd0ec76ba6da449
https://doi.org/10.2514/1.b37117
https://doi.org/10.2514/1.b37117
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::395e3d1ec5b42368c6e6f3b7acbd774c
https://doi.org/10.2514/6.2018-0885
https://doi.org/10.2514/6.2018-0885
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0832e995ca01c53b1310a8d50889d01d
https://doi.org/10.2514/6.2018-0401
https://doi.org/10.2514/6.2018-0401
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f88048b506be2e3a69eab28345039591
https://doi.org/10.2514/6.2017-1931
https://doi.org/10.2514/6.2017-1931
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::81bac278d60003cfb2322606171a7f99
https://doi.org/10.2514/6.2016-4978
https://doi.org/10.2514/6.2016-4978
Autor:
David P. Stechmann, Stephen D. Heister
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eabe9da51e270f037240ded08d23a44e
https://doi.org/10.2514/6.2016-1201
https://doi.org/10.2514/6.2016-1201
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
Autor:
David P. Stechmann, Stephen D. Heister
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Rotating detonation wave combustor (RDWC) technology and rotating detonation engines (RDEs) in general represents a promising concept for advancing beyond current thermodynamic and power density limits associated with traditional subsonic combustion
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::347d77e1ca82bf59fc7a963931474c16
https://doi.org/10.2514/6.2014-3902
https://doi.org/10.2514/6.2014-3902
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Hydrogen Peroxide (H2O2) bipropellant rocket engines have been in use since the 1950’s in launch vehicles, sounding rockets, and as RATO (Rocket Assisted TakeOff) units for aircraft. Often, these engines function at a low chamber pressure using pre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5636c393c26b30ea2458281058accc8b
https://doi.org/10.2514/6.2014-3500
https://doi.org/10.2514/6.2014-3500