An investigation was conducted to determine the aerodynamic characteristics of a tandem wing configuration. The configuration had a low forward mounted sweptback wing and a high rear mounted sweptforward wing jointed at the wing tip by an end plate. The investigation was conducted at a Mach number of 0.30 at angles of attack up to 20 deg. A comparison of the experimentally determined drag due to lift characteristics with theoretical estimates is also included. (Author)
Aerodynamic Characteristics of a Tandem Wing Configuration of a Mach Number of 0.30
1975
30 pages
Report
No indication
English
Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number
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