Add to ORKGThese calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, Germany, were based on the shape of the ZR III, with the following simplifications: cars, fins, and rudders removed; all cross sections replaced by equivalent circular cross sections. Under these assumptions the pressure distribution was calculated for the following cases: symmetrical case, or flow parallel to the axis; unsymmetrical case, or flow at an angle to the axis. In both cases the simple potential flow first forms the basis for the determination of the pressure distribution
The new method for making computations in connection with the study of rigid airships, which was use...
An outline of Von Karman's method of computing the potential flow of airships in yaw by means of par...
This is the third in a series of investigations of the water pressures on seaplane floats and hulls,...
These calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, German...
These calculations were based on the shape of the ZR III, with the following simplifications: cars, ...
This note, prepared for the National Advisory Committee for Aeronautics, contains the demonstration ...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
Differential and integral curves are presented and well as numerous calculations relating to hulls. ...
This report presents the results of measurements of pressure distribution conducted in the propeller...
The purpose of the first two parts of this report is to present in concise format all the formulas r...
In recent tests on the pressures occurring on the envelope and control surfaces of the naval airship...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...
The method of determining the pressure distribution on the fuselage is described, with special atten...
Pressure experimental data from NACA tests on the airship “Akron” were reanalysed in this study. The...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
The new method for making computations in connection with the study of rigid airships, which was use...
An outline of Von Karman's method of computing the potential flow of airships in yaw by means of par...
This is the third in a series of investigations of the water pressures on seaplane floats and hulls,...
These calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, German...
These calculations were based on the shape of the ZR III, with the following simplifications: cars, ...
This note, prepared for the National Advisory Committee for Aeronautics, contains the demonstration ...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
Differential and integral curves are presented and well as numerous calculations relating to hulls. ...
This report presents the results of measurements of pressure distribution conducted in the propeller...
The purpose of the first two parts of this report is to present in concise format all the formulas r...
In recent tests on the pressures occurring on the envelope and control surfaces of the naval airship...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...
The method of determining the pressure distribution on the fuselage is described, with special atten...
Pressure experimental data from NACA tests on the airship “Akron” were reanalysed in this study. The...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
The new method for making computations in connection with the study of rigid airships, which was use...
An outline of Von Karman's method of computing the potential flow of airships in yaw by means of par...
This is the third in a series of investigations of the water pressures on seaplane floats and hulls,...