Add to ORKGTests were made to determine the effect of fillets between wings and fuselage on the drag and propulsive efficiency of a high-wing cabin monoplane. These tests were made in the 20-foot Propeller Research Tunnel of the National Advisory Committee for Aeronautics
The drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various com...
As part of the wing-fuselage interference program in progress in the NACA variable-density wind tunn...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
This note describes tests made to determine the ef-fect of fillets between wings and fuselage on the...
Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by...
An investigation was conducted to determine the effect of the wings on propulsive efficiency. The wi...
The drag due to the various parts of a Fairchild (FC-2W2) cabin monoplane was measured at air speeds...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
Tests of a wing-fuselage combinations incorporating NACA 65-series airfoil sections were conducted i...
Some preliminary results of full scale wind tunnel testing to determine the best means of reducing t...
The effect of mutual propeller/nacelle of fuselage interference on aircraft propulsive efficiency is...
The drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various com...
As part of the wing-fuselage interference program in progress in the NACA variable-density wind tunn...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
This note describes tests made to determine the ef-fect of fillets between wings and fuselage on the...
Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by...
An investigation was conducted to determine the effect of the wings on propulsive efficiency. The wi...
The drag due to the various parts of a Fairchild (FC-2W2) cabin monoplane was measured at air speeds...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
Results of an investigation by the free-fall method are presented herein for a configuration having ...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
Tests of a wing-fuselage combinations incorporating NACA 65-series airfoil sections were conducted i...
Some preliminary results of full scale wind tunnel testing to determine the best means of reducing t...
The effect of mutual propeller/nacelle of fuselage interference on aircraft propulsive efficiency is...
The drag of a Sperry Messenger airplane with the wings removed, and also the drag of its various com...
As part of the wing-fuselage interference program in progress in the NACA variable-density wind tunn...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...