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Office National dEtudes et de Recherches Aerospatiales ONERA
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Office National dEtudes et de Recherches Aerospatiales ONERA
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Application filed by Office National dEtudes et de Recherches Aerospatiales ONERAfiledCriticalOffice National dEtudes et de Recherches Aerospatiales ONERA
Priority to FR918578ApriorityCriticalpatent/FR1350117A/fr
Application grantedgrantedCritical
Publication of FR1350117ApublicationCriticalpatent/FR1350117A/fr
B64C5/08—Stabilising surfaces mounted on, or supported by, wings
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Engineering & Computer Science
(AREA)
Aviation & Aerospace Engineering
(AREA)
FR918578A1962-12-131962-12-13Perfectionnements apportés aux aérodynes supersoniques à aile élancée, notamment à ceux à grand rayon d'action
ExpiredFR1350117A
(fr)
Aile d'aeronef permettant la rotation autour de l'axe de roulis par l'action de la pesanteur et comportant des dispositifs de controle de l'axe de lacet incorpores
Aile d'aeronef permettant la rotation autour de l'axe de roulis par l'action de la pesanteur et comportant des dispositifs de controle de l'axe de lacet incorpores
Application of low drag-due-to-lift concept of linearized theory to the studies of twist and camber of isolated wing and wing-body configurations of supersonic aircraft