Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Loral O'Hara"'
Autor:
Michael V. Jakuba, C. L. Taylor, Christopher Judge, Dana R. Yoerger, James C. Kinsey, Matthew Heintz, Jonathan C. Howland, Louis L. Whitcomb, Larry A. Mayer, C. Pontbriand, Carl L. Kaiser, Glenn McDonald, Christopher J. McFarland, Casey Machado, Christopher C. German, Stefano Suman, J. Bailey, Loral O'Hara, Andrew D. Bowen, Daniel Gomez-Ibanez
Publikováno v:
2014 Oceans - St. John's.
This paper reports the development of a new underwater robotic vehicle, Nereid-UI, with the goal of being capable of deployments in polar ocean regions traditionally considered difficult or impossible to access such the ice-ocean interface in margina
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bd1a9e3c6af3100c2118cecc30d5ad1
https://doi.org/10.1109/oceans.2014.7003125
https://doi.org/10.1109/oceans.2014.7003125
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The development of a velocity-based mechanistic combustion response model and its application to liquid rocket engines is described. A time lag model is applied to capture the periodic process of vortex shedding that is hypothesized to be the primary
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6521991f8713f1758510fb0264bcd1bd
https://doi.org/10.2514/6.2009-5136
https://doi.org/10.2514/6.2009-5136
Publikováno v:
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.
An experimental investigation of high-frequency longitudinal combustion instability using a continuously variable resonance combustor (CVRC) is described. The continuously variable resonance condition is provided by varying the length of a tube carry
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f220faa50902e26e765ae82eba054a1c
https://doi.org/10.2514/6.2009-234
https://doi.org/10.2514/6.2009-234
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
An experiment was designed to investigate the acoustically-induced vortex shedding process observed in liquid rocket engine combustion chambers. The experiment was developed by a Propulsion Design, Build, Test class at Purdue University as a prototyp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::222b444536b9480574970585677abd49
https://doi.org/10.2514/6.2008-4745
https://doi.org/10.2514/6.2008-4745