With the object of further clarifying the problem of spinning, the equilibrium of the forces and moments acting on an airplane is discussed in light of the most recent test data. Convinced that in a spin the flight attitude by only small angles of yaw is more or less completely steady, the study is primarily devoted to an investigation of steady spin with no side slip. At small angles, wholly arbitrary and perfectly steady spins may be forced, depending on the type of control displacements. But at large angles only very steep and only "approaching steady" spins are possible, no matter what the control displacements
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
Eight wings and three tails, covering a wide range of aerodynamic characteristics, were independentl...
In the Institute for Flight Mechanics of the DVL a reactor arrangement with a maximum output of 100 ...
This report deals first with the fundamental data required for the investigation. These are chiefly ...
Data from wind-tunnel tests on a model of the NY-1 airplane were used in a study of the effect on th...
With the object of further clarifying the problem of spinning, the equilibrium of the forces and mom...
This report deals with the autorotational characteristics of certain differing wing systems as deter...
The influence of different mathematical and aerodynamic models on computed spin motion was investiga...
This report presents the results of a series of autorotation and torque tests on four different rota...
Report presents the results of tests of a 1/10-scale model of the XN2Y-1 airplane tested in the NACA...
In this mathematical investigation, made in collaboration with Dr. Wilhelm Schmidt, we interpret the...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
An investigation was conducted in the Langley Spin Tunnel to measure the pressures on the surface of...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dyna...
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
Eight wings and three tails, covering a wide range of aerodynamic characteristics, were independentl...
In the Institute for Flight Mechanics of the DVL a reactor arrangement with a maximum output of 100 ...
This report deals first with the fundamental data required for the investigation. These are chiefly ...
Data from wind-tunnel tests on a model of the NY-1 airplane were used in a study of the effect on th...
With the object of further clarifying the problem of spinning, the equilibrium of the forces and mom...
This report deals with the autorotational characteristics of certain differing wing systems as deter...
The influence of different mathematical and aerodynamic models on computed spin motion was investiga...
This report presents the results of a series of autorotation and torque tests on four different rota...
Report presents the results of tests of a 1/10-scale model of the XN2Y-1 airplane tested in the NACA...
In this mathematical investigation, made in collaboration with Dr. Wilhelm Schmidt, we interpret the...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
An investigation was conducted in the Langley Spin Tunnel to measure the pressures on the surface of...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dyna...
A theoretical study was made of the angular motions of spinning bodies in space. The analysis was ba...
Eight wings and three tails, covering a wide range of aerodynamic characteristics, were independentl...
In the Institute for Flight Mechanics of the DVL a reactor arrangement with a maximum output of 100 ...