ES239702U - Un perfil aerodinamico de ala para aviacion - Google Patents

Un perfil aerodinamico de ala para aviacion

Info

Publication number
ES239702U
ES239702U ES1978239702U ES239702U ES239702U ES 239702 U ES239702 U ES 239702U ES 1978239702 U ES1978239702 U ES 1978239702U ES 239702 U ES239702 U ES 239702U ES 239702 U ES239702 U ES 239702U
Authority
ES
Spain
Prior art keywords
curvature
aviation
translation
machine
legally binding
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
ES1978239702U
Other languages
English (en)
Other versions
ES239702Y (es
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space SA
Original Assignee
Construcciones Aeronauticas CASA SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Construcciones Aeronauticas CASA SA filed Critical Construcciones Aeronauticas CASA SA
Priority to ES1978239702U priority Critical patent/ES239702Y/es
Publication of ES239702U publication Critical patent/ES239702U/es
Application granted granted Critical
Publication of ES239702Y publication Critical patent/ES239702Y/es
Expired legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Un perfil aerodinámico de ala para aviación que está específicamente diseñado para volar en régimen transónico, caracterizado porque su contorno presenta en su parte superior o extradós una curvatura convexa con una posición determinada del punto de curvatura mínima y su aumento continuo de la curvatura a partir de el para asegurar la estabilización de la capa límite; en su parte inferior o intradós está constituido por un tramo curvo-convexo y en otro tramo posterior curvo-cóncavo que dan curvatura al borde de salida de manera que el perfil necesita una, incidencia menor durante el vuelo, permitiendo todo ello que los efectos de divergencia se presenten a un número de energía y a una reducción en el costo directo de operción por disminuirse el valor del coeficiente de resistencia al avance, así como a mejores actuaciones de vuelo para una potencia dada.
ES1978239702U 1978-11-24 1978-11-24 Un perfil aerodinamico de ala para aviacion Expired ES239702Y (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES1978239702U ES239702Y (es) 1978-11-24 1978-11-24 Un perfil aerodinamico de ala para aviacion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES1978239702U ES239702Y (es) 1978-11-24 1978-11-24 Un perfil aerodinamico de ala para aviacion

Publications (2)

Publication Number Publication Date
ES239702U true ES239702U (es) 1979-01-01
ES239702Y ES239702Y (es) 1979-05-16

Family

ID=8399794

Family Applications (1)

Application Number Title Priority Date Filing Date
ES1978239702U Expired ES239702Y (es) 1978-11-24 1978-11-24 Un perfil aerodinamico de ala para aviacion

Country Status (1)

Country Link
ES (1) ES239702Y (es)

Also Published As

Publication number Publication date
ES239702Y (es) 1979-05-16

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