Zobrazeno 1 - 10
of 41
pro vyhledávání: '"Nicolas Hamel"'
Autor:
Stephen Jackson
Publikováno v:
Notes and Queries. :540-541
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f28c2ccbafcb49cbabdd67e0a279871
https://doi.org/10.1093/nq/s4-vi.156.540b
https://doi.org/10.1093/nq/s4-vi.156.540b
Autor:
James Gilbert
Publikováno v:
Notes and Queries. :64-64
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce089498d543f3f6b5c05010edf00fd5
https://doi.org/10.1093/nq/s4-vii.160.64a
https://doi.org/10.1093/nq/s4-vii.160.64a
Autor:
Ryan Luciano, Robert Desaulnier, Antoine Despeyroux, Jean-Pierre Hickey, Michael Piotrowski, Nicolas Hamel
Publikováno v:
Journal of Spacecraft and Rockets. 52:1236-1252
Grid fins provide good maneuverability to missiles in supersonic flow because they can maintain lift at a higher angle of attack. Although static aerodynamic data exist, very little quantitative dynamic performance information is available for grid f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee11afede795465f1fad40a4e6c3299b
https://doi.org/10.2514/1.a33189
https://doi.org/10.2514/1.a33189
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:
Mahmood Khalid, Weixing Yuan, Francois Lesage, Nicolas Hamel, Patrick Zdunich, Xingzhong Huang
Publikováno v:
26th AIAA Applied Aerodynamics Conference.
26th AIAA Applied Aerodynamics Conference (from 8/18/2008 to 8/21/2008)
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unclassified
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unlimited
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b4c8079ede54dfce898a69ea73d545dc
https://doi.org/10.2514/6.2008-6396
https://doi.org/10.2514/6.2008-6396
Publikováno v:
25th AIAA Applied Aerodynamics Conference.
The field of artillery must meet ever more stringent operational needs in the delivery of precise effects. Closely connected to meet these needs for the Canadian Forces, DRDC Valcartier studies solutions of guidance and control. DRDC Valcartier under
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a67e22282ddd1e59d8d8e6e4ce11337c
https://doi.org/10.2514/6.2007-4075
https://doi.org/10.2514/6.2007-4075
Publikováno v:
45th AIAA Aerospace Sciences Meeting and Exhibit.
A multi-disciplinary project was undertaken at DRDC Valcartier with the objective of developing a control actuation system that could be embedded in the structure of a missile to provide measurable control authority through boundary layer and vortex
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41a5f331fe6b9ba6c39d549d3073e816
https://doi.org/10.2514/6.2007-273
https://doi.org/10.2514/6.2007-273
Publikováno v:
24th AIAA Applied Aerodynamics Conference.
Using nose-mounted micro-structures, it was shown experimentally and computationally in earlier publications by the authors that signiflcant side force could be generated at moderate angles-of-attack and for supersonic ∞ow on a generic missile conf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff84ed5d72a3182219fc5caa7e5f75fa
https://doi.org/10.2514/6.2006-3000
https://doi.org/10.2514/6.2006-3000
Publikováno v:
23rd AIAA Applied Aerodynamics Conference.
The aim of this study is to evaluate computationall y the aerodynamic forces generated on a generic missile configuration through vortex manipulation using square-edged rectangular micro-flow effectors mounted at a distance of 0.84 caliber from the n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94f6a6a6027710f0b8e693d9b5547db4
https://doi.org/10.2514/6.2005-4968
https://doi.org/10.2514/6.2005-4968
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::23913f099d8219699ea5d622c10144d2
https://doi.org/10.2514/6.2003-5238
https://doi.org/10.2514/6.2003-5238