Zobrazeno 1 - 10
of 133
pro vyhledávání: '"Anjaneyulu Krothapalli"'
Autor:
Anjaneyulu Krothapalli
Publikováno v:
International Journal of Aeroacoustics. 21:307-314
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72c70e4de851e0c6b0e5c8641bf115b6
https://doi.org/10.1177/1475472x221107373
https://doi.org/10.1177/1475472x221107373
Publikováno v:
Energy Procedia. 57:2762-2771
The Multiple Parabolic Reflector Flat Plate Collector (MPFC) is designed to concentrate solar energy while remaining stationary. Inside the panel is an array of parabolic trough reflectors with tubular receivers. The receiver array transverses within
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a747f8ff0a58c6b7b894f347f4ed16df
https://doi.org/10.1016/j.egypro.2014.10.308
https://doi.org/10.1016/j.egypro.2014.10.308
Publikováno v:
International Journal of Hydrogen Energy. 38:11790-11798
This paper presents the results from an experimental study on the energy conversion efficiency of producing hydrogen enriched syngas through uncatalyzed steam biomass gasification. Wood pellets wer ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::56c65871dd83a8a97bd1aac14fc524a1
https://doi.org/10.1016/j.ijhydene.2013.07.022
https://doi.org/10.1016/j.ijhydene.2013.07.022
(AIAA Paper 87-0248), Journal of Propulsion and Power, Vol. 7, No. 3, May-Jun. 1991. Air Force Office of Scientific Research under Contract F 49620-79-0189 Air Force Office of Scientific Research under Contract F 49620-79-0189
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::408da2c75ca3f0d485f32c11adfc36fb
https://hdl.handle.net/10945/50064
https://hdl.handle.net/10945/50064
Publikováno v:
Journal of Propulsion and Power. 28:293-306
An experimental study is carried out to investigate the characteristics of a pulsed-jet ejector thrust augmentor that is suitable for use in vertical take-off and landing aircraft. Phase-locked particle image velocimetry is used to obtain the detaile
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e5f9aa01470cb7d06dd7d5378e5b110
https://doi.org/10.2514/1.43233
https://doi.org/10.2514/1.43233
Autor:
M. J. Czech, Krishna Viswanathan, John M. Seiner, Anjaneyulu Krothapalli, Bernard J. Jansen, Brenton Greska
Publikováno v:
Journal of Aircraft. 48:412-423
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1731d4ebfb00917856b6174640a73657
https://doi.org/10.2514/1.c000285
https://doi.org/10.2514/1.c000285
Publikováno v:
AIAA Journal. 48:1256-1261
P ULSED jets have a variety of applications ranging form pulsing blood flow in the human heart (Gharib et al. [1]) to pulseddetonation engines (PDEs). The first application of a pulsed-jet engine was during the World War II for propelling a flying/bu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2949dc259c3845044dabaf8c4a50d143
https://doi.org/10.2514/1.j050026
https://doi.org/10.2514/1.j050026
Publikováno v:
Journal of Fluid Mechanics. 631:23-63
An experimental study is carried out to elucidate the structure of a high Reynolds number (~105) turbulent pulsed jet. Particle image velocimetry measurements showed that the near flow field is dominated by a series of vortex rings with jet-like flow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f7ba9d566fd90fa7623e1089c3c934c
https://doi.org/10.1017/s0022112009007009
https://doi.org/10.1017/s0022112009007009
Publikováno v:
Journal of Fluid Mechanics. 578:139-169
The role of the streamwise vortices on the aeroacoustics of a Mach 0.9 axisymmetric jet is investigated using two different devices to generate streamwise vortices: microjets and chevrons. The resultant acoustic field is mapped by sideline microphone
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3ff571b0d432b28ead44468d6543137
https://doi.org/10.1017/s0022112007005022
https://doi.org/10.1017/s0022112007005022
Publikováno v:
AIAA Journal. 45:793-805
A way of controlling the acoustic and aerodynamic characteristics of ideally expanded impinging twin jets has been proposed. As a means of control, microjets were used at the nozzle exit. The effect of the controlling method on the flowfield and acou
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::947f84909b08fdaaa3ebdb257b219c42
https://doi.org/10.2514/1.19914
https://doi.org/10.2514/1.19914