Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Wesly S. Anderson"'
Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine
Publikováno v:
Journal of Propulsion and Power. 36:851-861
A liquid bipropellant rotating detonation rocket engine was successfully test fired. The 6.5-in.-diam engine operates on a mixture of rocket-grade hydrogen peroxide and triglyme. Ignition is accomp...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c535c494c73246aaaf939f0825f1ec6f
https://doi.org/10.2514/1.b37666
https://doi.org/10.2514/1.b37666
Autor:
Stephen D. Heister, Wesly S. Anderson
Publikováno v:
Journal of Propulsion and Power. 35:303-312
A bench-scale experiment was developed to investigate the response of a liquid injector site to the passage of multiple-detonation-type events with application to rotating detonation engines. The e...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e3f2916f9a5bcd455bfe075c7eea388
https://doi.org/10.2514/1.b37127
https://doi.org/10.2514/1.b37127
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0fbcf8421a506d400d6ab733d4f4daf
https://doi.org/10.2514/6.2020-0196
https://doi.org/10.2514/6.2020-0196
Autor:
Stephen D. Heister, Wesly S. Anderson
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
A bench-scale experiment was developed to investigate the response of a liquid injector site to the passage of multiple-detonation-type events with application to rotating detonation engines. The e...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2d8be44fc2ab403c2df4f8f979eeefb
https://doi.org/10.2514/6.2018-0635
https://doi.org/10.2514/6.2018-0635
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
Autor:
Marc D. Polanka, Cheng-Xian Lin, Wesly S. Anderson, Balu Sekar, Scott D. Stouffer, Dave S. Evans, Joseph Zelina
Publikováno v:
Journal of Propulsion and Power. 27:257-268
Marc D. Polanka,∗ Joseph Zelina,∗ Wesly S. Anderson, and Balu Sekar∗ U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433 Dave S. Evans Air Force Institute of Technology, Wright-Patterson Air Force Base, Ohio 45433 Ch
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::643ee82f777409daf6de2fa1ee172dc2
https://doi.org/10.2514/1.45317
https://doi.org/10.2514/1.45317
Publikováno v:
Volume 5A: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Microturbines, Turbochargers, and Small Turbomachines.
A small gas turbine performance modeling and testing project has been completed as part of a DSTO research program. The main objective of the program was to enhance capability in understanding and modeling the thermodynamic and performance characteri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc64a5b2808259bc7d53834ef2ed4dd1
https://doi.org/10.1115/gt2013-94405
https://doi.org/10.1115/gt2013-94405
Autor:
Wesly S. Anderson, Wright-Patterson Afb, Balu Sekar, Richard Jack Holder, Joseph Zelina, Alejandro M. Briones, Cheng-Xian Lin, Scott D. Stouffer, Marc D. Polanka, Hugh Thornburg
Publikováno v:
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
Film cooling plays a critical role in providing effective thermal protection to components in modern gas turbine engines. Most of the previous computational studies on film cooling were conducted using cylindrical or shaped coolant holes with pure cr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::82ef1b80f12202361c4f7eddaf57aff1
https://doi.org/10.2514/6.2009-678
https://doi.org/10.2514/6.2009-678
Autor:
Marc D. Polanka, Wesly S. Anderson, Garth R. Justinger, Scott D. Stouffer, Dave S. Evans, Joseph Zelina
Publikováno v:
Volume 3: Heat Transfer, Parts A and B.
Film cooling plays a critical role in providing effective thermal protection to components in modern gas turbine engines. A significant effort has been undertaken over the last 40 years to improve the distribution of coolant and to ensure that the ai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2f43646898c32cce69b89d1eac9cc4c1
https://doi.org/10.1115/gt2009-59242
https://doi.org/10.1115/gt2009-59242