Zobrazeno 1 - 10
of 19
pro vyhledávání: '"W.H.C. Halswijk"'
Autor:
W.H.C. Halswijk, B. van Zelderen, R.G. Veraar, H.M.A. Schleijpen, S.A. van Binsbergen, F. Bouquet
Publikováno v:
Target and Background Signatures III.
In performance prediction of IR sensor systems for missile detection, apart from the sensor specifications, target signatures are essential variables. Very often, for velocities up to Mach 2-2.5, a simple model based on the aerodynamic heating of a p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::34eba9c4bbafd015678976b141ac19e5
https://doi.org/10.1117/12.2276943
https://doi.org/10.1117/12.2276943
Autor:
W.H.C. Halswijk
Publikováno v:
AIAA Guidance, Navigation, and Control Conference and Exhibit, 10-13 August 2009, Chicago, IL, USA (Conference code: 81960)
The Variable-Flow Ducted Rocket (VFDR) is a type of ramjet that can control the fuel mass flow to the combustion chamber. It combines the high efficiency at high-speed of ramjets with the throttlability of turbofans, and this makes VFDR propulsion an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b94119e53bd0d18ce90555ac7f817ac7
http://resolver.tudelft.nl/uuid:fbbe8367-3695-4bd0-b99c-b0ba388cb4fd
http://resolver.tudelft.nl/uuid:fbbe8367-3695-4bd0-b99c-b0ba388cb4fd
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
Publikováno v:
ICMENS
A microscale thruster, has been successsfully designed using MEMS technology, in that 'stacked wafer' design is adopted.The thruster is built up of stacked and bonded silicon wafer, each with its own internal structure. The MEMS technology as succeed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2616f94cd91380bdbea1247daf0500ee
https://doi.org/10.1109/icmens.2005.124
https://doi.org/10.1109/icmens.2005.124
Publikováno v:
AIAA Modeling and Simulation Technologies Conference and Exhibit.
A model was developed to predict the thrust of throttled ramjet propelled missiles. The model is called DRCORE and fulfils the growing need to predict the performance of air breathing missiles. Each subsystem of the propulsion unit of this model is c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b1ce4fc457cf9a957bbdb3925e1d60c
https://doi.org/10.2514/6.2005-6013
https://doi.org/10.2514/6.2005-6013
Autor:
W.H.C. Halswijk, J.L.P.A. Moerel
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference and Exhibit 2005, San Francisco, CA, USA, 15-18 August 2005 (Conference code: 66314), 215-233
Many countries are developing technologies for future hypersonic air breathing cruise missiles. These missiles are foreseen to be employed against, amongst others, deeply buried targets. The main technological challenges are related to severe aerodyn
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ebbc44174306321511741b471f2247ce
http://resolver.tudelft.nl/uuid:a0b7a88a-09c9-44e6-9e9a-432856aea4e5
http://resolver.tudelft.nl/uuid:a0b7a88a-09c9-44e6-9e9a-432856aea4e5
Publikováno v:
AIAA Modeling and Simulation Technologies Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::787bec0a65eeb5ca530f9e587755b19b
https://doi.org/10.2514/6.2001-4413
https://doi.org/10.2514/6.2001-4413
Autor:
R.M. van der Horst, Marc Lauzon, Robert Stowe, J.L.P.A. Moerel, W.H.C. Halswijk, R.F. Calzone
Publikováno v:
AIAA Modeling and Simulation Technologies Conference and Exhibit.
The Netherlands defence research organisation TNO Prins Maurits Laboratory (TNO-PML) and the Defence Research Establishment Valcartier (DREV) in Canada maintain missile technology knowledge bases that are continuously being updated by means of resear
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2651c98baaac15d89e0ad07ae8670123
https://doi.org/10.2514/6.2001-4412
https://doi.org/10.2514/6.2001-4412
Autor:
James P.R. Day, W.H.C. Halswijk, Adam D. Devir, Justin Huneault, Jason Loiseau, Jimmy Verreault, Andrew J. Higgins
Publikováno v:
Procedia Engineering. :618-627
Laboratory experiments of hypervelocity impacts on aluminum, nylon and high-explosive targets are presented. Spectral measurements of the impact flash are recorded, together with radiometric measurements to derive the temperature of the flash. Such e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0bdd67a7a0331d6e6d0f56ffb62cbef8
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