MAQUETA DE AERONAVE PARA TUNEL DE VIENTO CON ALA TRUNCADA

MAQUETA DE AERONAVE PARA TUNEL DE VIENTO CON ALA TRUNCADA

An aircraft model for testing in a wind tunnel of width W including a fuselage, a truncated wing whose length L1 is less than the length L of a full scaled wing and additional components in the rear of the aircraft as, in particular, a horizontal tail plane, that produces the same downwash that arri...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: VELA ORGE, PILAR, PASCUAL FUERTES, ANGEL, AMO GARRIDO, ESTEBAN
Format: Patent
Sprache:spa
Schlagworte:
MEASURING
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
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Beschreibung
Zusammenfassung:An aircraft model for testing in a wind tunnel of width W including a fuselage, a truncated wing whose length L1 is less than the length L of a full scaled wing and additional components in the rear of the aircraft as, in particular, a horizontal tail plane, that produces the same downwash that arrives to the additional components as in a full scaled model. The shape of the truncated wing may be designed for having a similar lift distribution to the lift distribution of a full scaled wing along at least the maximum length L2 in the Y-axis of any component in the rear of the aircraft. The invention also relates to a method for designing the truncated wing.