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pro vyhledávání: '"Ronald Veraar"'
Autor:
Ronald Veraar
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
By injecting and mixing the fuel upstream of the combustor and initiating the combustion of the fuel-air mixture by a shock wave in the combustor, shock-induced combustion ramjets offer the potential to drastically reduce the length and mass of scram
Autor:
Nicolas Hamel, Rogerio Pimentel, Jan Vos, Francois Lesage, J.L.P.A. Moerel, Ronald Veraar, Daniel Corriveau, W.H.C. Halswijk
Publikováno v:
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver, CO, USA, 2-5 August 2009 (Conference code: 81720)
Two research institutes TNO Defence, Security and Safety and DRDC-Valcartier have worked together on the improvement of modeling and simulation tools for the functioning of supersonic air intakes for realistic ramjet engines of tactical missiles. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::976f027e473c5f001a11f0384168bf6d
http://resolver.tudelft.nl/uuid:77e5543e-e906-4b79-aa02-dc27f3d23393
http://resolver.tudelft.nl/uuid:77e5543e-e906-4b79-aa02-dc27f3d23393
Autor:
Alfons Mayer, Ronald Veraar, Rocco Farinaccio, Robert Stowe, Paul Harris, Alain deChamplain, Jimmy Verreault
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
This work presents a design for a shock-induced combustion experiment using a two-angle cone configuration. Three injector geometries were considered: a cone surface, a dual stage configuration with rectangular gaps (DSRG) and a cylindrical ramp (CR)