Add to ORKGTests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of the interference effects and drag of struts on a monoplane. Inclined struts were placed upon a Gottingen 387 airfoil in the lower surface positions and in two upper surface positions. Tests were made at values of Reynolds Number comparable with those obtained in flight. It was found that the interference drag of struts may be as great as the drag of the struts alone
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
This report deals with a description and report of tests carried out at the Washington Navy Yard on ...
This report deals with the results of tests on struts conducted at Washington Navy Yard. Two models ...
Tests were conducted to determine the importance of the interference effects and drag of struts on a...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
In the first series of wind tunnel tests, the drag and cross wing force of all the struts were measu...
This report presents the second of two studies under the same title. In this part five theoretical s...
As part of the wing-fuselage interference program in progress in the NACA variable-density wind tunn...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
Some preliminary results of full scale wind tunnel testing to determine the best means of reducing t...
This report contains the results of a series of tests with three wing models. By changing the sectio...
This report presents a detailed examination of the factors that went into the design of the Stipa mo...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
This report deals with a description and report of tests carried out at the Washington Navy Yard on ...
This report deals with the results of tests on struts conducted at Washington Navy Yard. Two models ...
Tests were conducted to determine the importance of the interference effects and drag of struts on a...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
In the first series of wind tunnel tests, the drag and cross wing force of all the struts were measu...
This report presents the second of two studies under the same title. In this part five theoretical s...
As part of the wing-fuselage interference program in progress in the NACA variable-density wind tunn...
This report gives the results of an investigation of the mutual interference of an airfoil and a fla...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
Three groups of airfoils have been tested in the variable density wind tunnel. The first group conta...
Some preliminary results of full scale wind tunnel testing to determine the best means of reducing t...
This report contains the results of a series of tests with three wing models. By changing the sectio...
This report presents a detailed examination of the factors that went into the design of the Stipa mo...
An investigation of the interference associated with tail surfaces added to wing-fuselage combinatio...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
This report deals with a description and report of tests carried out at the Washington Navy Yard on ...
This report deals with the results of tests on struts conducted at Washington Navy Yard. Two models ...