Add to ORKGThis report presents a detailed examination of the factors that went into the design of the Stipa monoplane. The model tested in the wind tunnel was made dissymmetrical externally, in order to produce a lift even at an angle of attack of 0 degrees with respect to the longitudinal axis of the tube
Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
The maximum lift coefficient for the airplane is compared with that obtained for the Gottingen 387 a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
This report presents a detailed examination of the factors that went into the design of the Stipa mo...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
Comparative flight tests were made with a small parasol monoplane in which the aerodynamic character...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
The drag due to the various parts of a Fairchild (FC-2W2) cabin monoplane was measured at air speeds...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
The maximum lift coefficient for the airplane is compared with that obtained for the Gottingen 387 a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
This report presents a detailed examination of the factors that went into the design of the Stipa mo...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
Comparative flight tests were made with a small parasol monoplane in which the aerodynamic character...
Tests were made to determine the effect of fillets between wings and fuselage on the drag and propul...
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
The drag due to the various parts of a Fairchild (FC-2W2) cabin monoplane was measured at air speeds...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
Force tests on a systematic series of wing systems over a range of angle of attack from minus forty-...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
Model tests prove the feasibility of enhancing the aerodynamic qualities of wing-fuselage fillets by...
This preliminary report furnishes information on the changes in the forces on each wing of a biplane...
The maximum lift coefficient for the airplane is compared with that obtained for the Gottingen 387 a...