The present article, which constitutes a continuation of the work of Von Baumhauer and Konig, will therefore be restricted to the fluttering of the tail surfaces and especially to oscillations of the horizontal empennage. This will also illustrate the characteristics of all other phenomena of fluttering
Investigation of damping in roll within range of maximum lift with the Albatross L 75, with and with...
A definition of "stalled fight" is presented as well as a detailed discussion on the how and why it ...
Formulas are given for the propelling or drag force experience in a uniform air stream by an airfoil...
On various low-wing monoplanes the horizontal tail surfaces flutter in flight at large angles of att...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
After an incident which, it was suspected, was due to symmetric elevator flutter, had occurred on t...
This report gives the results of a detailed study of the flutter characteristics of four representat...
This report presents a survey of previous theoretical and experimental investigations on wing flutte...
During a flight with a Van Berkel W. B. seaplane it was observed that the wing could perform violent...
The present paper is a continuation of the general study of flutter published in NACA reports nos. 4...
Tests of several modern airplanes indicate that control surfaces with a high degree of aerodynamic b...
In the course of a flight test of a supersonic research pilotless aircraft (the NACA RM-1), large-am...
This investigation covers only that phase of airplane accidents which are the result of sideslip. We...
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured ...
In this report a study is made of the effect on longitudinal and lateral oscillations of an airplane...
Investigation of damping in roll within range of maximum lift with the Albatross L 75, with and with...
A definition of "stalled fight" is presented as well as a detailed discussion on the how and why it ...
Formulas are given for the propelling or drag force experience in a uniform air stream by an airfoil...
On various low-wing monoplanes the horizontal tail surfaces flutter in flight at large angles of att...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
After an incident which, it was suspected, was due to symmetric elevator flutter, had occurred on t...
This report gives the results of a detailed study of the flutter characteristics of four representat...
This report presents a survey of previous theoretical and experimental investigations on wing flutte...
During a flight with a Van Berkel W. B. seaplane it was observed that the wing could perform violent...
The present paper is a continuation of the general study of flutter published in NACA reports nos. 4...
Tests of several modern airplanes indicate that control surfaces with a high degree of aerodynamic b...
In the course of a flight test of a supersonic research pilotless aircraft (the NACA RM-1), large-am...
This investigation covers only that phase of airplane accidents which are the result of sideslip. We...
The damping in yaw and the directional stability of a model freely oscillating in yaw were measured ...
In this report a study is made of the effect on longitudinal and lateral oscillations of an airplane...
Investigation of damping in roll within range of maximum lift with the Albatross L 75, with and with...
A definition of "stalled fight" is presented as well as a detailed discussion on the how and why it ...
Formulas are given for the propelling or drag force experience in a uniform air stream by an airfoil...