Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Luca M. L. Cantu"'
Autor:
Luca M. L. Cantu, Emanuela C. A. Gallo
Publikováno v:
The European Physical Journal Plus. 137
Ultraviolet Raman spectroscopy measurements have been taken to detect non-uniform and self-prepared samples of both explosives and warfare agent simulants on realistic backgrounds. The main goal was to quantify the minimum requirements for an unambig
Publikováno v:
Optical Engineering. 60
Deep ultraviolet Raman spectroscopy measurements have been performed at the German Aerospace Center (DLR) with the aim of detecting traces (µg range) of explosive precursors. In this study a backscattering Raman system was set up and optimized to de
Autor:
Nadeshda A. Slavinskaya, Trupti Kathrotia, Manfred Aigner, Wolfgang Meier, Patrick Le Clercq, Luca M. L. Cantu, Jasper Grohmann, Michael Rachner, Georg Eckel
Publikováno v:
Combustion and Flame. 207:134-152
Due to the introduction of alternative aviation fuels, new methods and models are necessary which have the capability to predict the performance of combustors dependent on the fuel composition. Towards this target, a multi-component vaporization mode
Autor:
Christopher P. Goyne, Luca M. L. Cantu, Andrew D. Cutler, Emanuela Gallo, Gaetano Magnotti, Robert D. Rockwell
Publikováno v:
AIAA Journal. 57:313-326
Dual-pump coherent anti-Stokes Raman spectroscopy (CARS) was used to measure the mole fractions of major species as well as the rotational and vibrational temperatures of molecular nitrogen in a hy...
Autor:
Robert D. Rockwell, Jack R. Edwards, Christopher P. Goyne, Harsha K. Chelliah, Andrew D. Cutler, Brian E. Rice, Luca M. L. Cantu, Paul M. Danehy, James C. McDaniel, Emanuela C. A. Gallo
Publikováno v:
J Propuls Power
Hypersonic air-breathing engines rely on scramjet combustion processes, which involve high-speed, compressible, and highly turbulent reacting flows. The combustion environment and the turbulent flames at the heart of these engines are difficult to si
Ultraviolet Raman spectroscopy measurements have been taken at DLR in Lampoldshausen to detect NATO SET-237 standard samples of RDX. The main goal was to quantify the minimum requirements for an unambiguous identification in remote detection (60 cm d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f49c393f8d4e5870d9cbd0f79e7998c7
https://elib.dlr.de/141159/
https://elib.dlr.de/141159/
Autor:
Emanuela C. A. Gallo, Robert D. Rockwell, Luca M. L. Cantu, James C. McDaniel, Justin W. Kirik, Christopher P. Goyne, Andrew D. Cutler
Publikováno v:
Journal of Propulsion and Power. 34:739-749
Particle image velocimetry was performed in the spanwise centerplane of a scramjet cavity flameholder under premixed hydrocarbon-fueled dual-mode conditions, providing the first reported results of...
Autor:
Christopher P. Goyne, Luca M. L. Cantu, Emanuela C. A. Gallo, Robert D. Rockwell, Andrew D. Cutler
Publikováno v:
Combustion and Flame. 189:92-105
As part of a broader effort to provide detailed measurements of turbulent flames in dual-mode scramjets, promote a deeper understanding of the relevant combustion physics, and aid appropriate computational model development, a high-subsonic cavity-st
Autor:
Emanuela C. A. Gallo, Paul M. Danehy, Luca M. L. Cantu, Christopher P. Goyne, Colin D. McRae, Craig T. Johansen, Andrew D. Cutler, Robert D. Rockwell, James C. McDaniel
Publikováno v:
Journal of Propulsion and Power. 32:542-559
Flow visualization and statistical analysis of a supersonic, turbulent reacting flow from nonintrusive hydroxyl radical planar laser-induced fluorescence images are presented. The OH-PLIF images show instantaneous structures of turbulence in two comb
Autor:
Emanuela C. A. Gallo, Paul M. Danehy, Brett F. Bathel, Luca M. L. Cantu, James C. McDaniel, Andrew D. Cutler, Robert D. Rockwell, Christopher P. Goyne
Publikováno v:
Journal of Propulsion and Power. 32:373-382
Nitric oxide planar laser-induced fluorescence measurements have been performed in a small-scale scramjet combustor at the University of Virginia Aerospace Research Laboratory at nominal simulated Mach 5 flight. A mixture of nitric oxide and nitrogen