WIND TUNNEL AIRCRAFT MODEL WITH TRUNCATED WING

An aircraft model (17) for testing in a wind tunnel (11) of width W comprising a fuselage (21), a truncated wing (25) whose length L1 is lesser than the length L of a full scaled wing (23) and additional components in the rear aircraft as, in particular, an horizontal tail plane (29), that produces...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GARRIDO ESTEBAN AMO, FUERTES ANGEL PASCUAL, ORGE PILAR VELA
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CALCULATING COMPUTING COSMONAUTICS COUNTING ELECTRIC DIGITAL DATA PROCESSING HELICOPTERS PERFORMING OPERATIONS PHYSICS TRANSPORTING
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