IT1145832B - Unione per rotazione di pezzi stampati in lamiera
- Google Patents
Unione per rotazione di pezzi stampati in lamiera
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Publication number
IT1145832B
IT1145832BIT04808/81AIT480881AIT1145832BIT 1145832 BIT1145832 BIT 1145832BIT 04808/81 AIT04808/81 AIT 04808/81AIT 480881 AIT480881 AIT 480881AIT 1145832 BIT1145832 BIT 1145832B
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Priority claimed from DE19803006514external-prioritypatent/DE3006514A1/de
Priority claimed from DE19803038633external-prioritypatent/DE3038633A1/de
Priority claimed from DE19803040705external-prioritypatent/DE3040705A1/de
Application filed by Leistritz Hans KarlfiledCriticalLeistritz Hans Karl
Publication of IT8104808A0publicationCriticalpatent/IT8104808A0/it
Application grantedgrantedCritical
Publication of IT1145832BpublicationCriticalpatent/IT1145832B/it
F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
F05C2201/00—Metals
F05C2201/02—Light metals
F05C2201/021—Aluminium
Landscapes
Pressure Welding/Diffusion-Bonding
(AREA)
IT04808/81A1980-02-211981-02-20Unione per rotazione di pezzi stampati in lamiera
IT1145832B
(it)
Calculation of the drag of fuselage tail sections of different shapes in supersonic flow of a nonviscous gas(Raschet soprotivleniia khvostovykh chastei fiuzeliazhei razlichnykh form pri obtekanii sverkhzvukovym potokom neviazkogo gaza)
Entree d'air supersonique en demi-corps de revolution pour propulseurs a reaction, notamment pour moteurs-fusees du type statoreacteur a propergols solides