This note, prepared for the National Advisory Committee for Aeronautics, contains the demonstration that the pressure around the circular cross section of an elongated airship, plotted against the diameter of symmetry, can be expected to be represented by a straight line
A model of the C class airship hull, when severed at its major section and provided with a cylindric...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
These calculations were based on the shape of the ZR III, with the following simplifications: cars, ...
These calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, German...
These calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, German...
This note, prepared for the National Advisory Committee for Aeronautics, contains the demonstration ...
In recent tests on the pressures occurring on the envelope and control surfaces of the naval airship...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
The laws of curvilinear motion are established and the transverse forces on elongated airship hulls ...
The circular motion for airship-like bodies has thus far been calculated only for a prolate ellipsoi...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
In recent tests on the pressures occurring on the envelope and control surfaces of the naval airship...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
A model of the C class airship hull, when severed at its major section and provided with a cylindric...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
These calculations were based on the shape of the ZR III, with the following simplifications: cars, ...
These calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, German...
These calculations, made at the request of the Zeppelin Airship Company of Friederichshafen, German...
This note, prepared for the National Advisory Committee for Aeronautics, contains the demonstration ...
In recent tests on the pressures occurring on the envelope and control surfaces of the naval airship...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
The laws of curvilinear motion are established and the transverse forces on elongated airship hulls ...
The circular motion for airship-like bodies has thus far been calculated only for a prolate ellipsoi...
This investigation was made for the purpose of determining the aerodynamic pressure distribution enc...
This note, prepared for the National Advisory Committee for Aeronautics, contains a discussion of th...
In recent tests on the pressures occurring on the envelope and control surfaces of the naval airship...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
A model of the C class airship hull, when severed at its major section and provided with a cylindric...
The pressure distribution over ellipsoids when in translatory motion through a perfect fluid is calc...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
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