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
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
The results presented in this note show the effect of twist and sweepback on the span load distribut...
This report presents a detailed examination of the factors that went into the design of the Stipa mo...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This reports presents the results of pressure distribution tests on a thick, tapered and twisted mon...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
The present report deals with a number of problems, particularly with the interaction of the fuselag...
The NACA 23012-4 airfoil was investigated for the purpose of increasing lift by means of blowing out...
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
The results presented in this note show the effect of twist and sweepback on the span load distribut...
This report presents a detailed examination of the factors that went into the design of the Stipa mo...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
Tests were conducted in the Variable Density Wind Tunnel of the NACA to determine the importance of ...
In the following we develop a non-autorotating monoplane wing. The conditions imposed on such a wing...
This investigation covers force tests through a large range of angle of attack on a series of monopl...
This reports presents the results of pressure distribution tests on a thick, tapered and twisted mon...
This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with win...
In the foregoing remarks I have made an attempt to touch on some of the structural problems met with...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
The present report deals with a number of problems, particularly with the interaction of the fuselag...
The NACA 23012-4 airfoil was investigated for the purpose of increasing lift by means of blowing out...
Report presents the results of an experimental investigation made in the NACA full-scale wind tunnel...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
The results presented in this note show the effect of twist and sweepback on the span load distribut...