Add to ORKGA simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This criterion is intended to be used, much like the Naval Architect's standard wave, for preliminary estimates of longitudinal strength requirements. It should be useful in tradeoff studies between speed, fineness ratio, block coefficient, structure weight, and other such general parameters of airship design
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
The author describes experiments in designing nonrigid airships. A nonrigid airship of 32,000 cubic ...
This report describes the theory of calculating the principal stresses in the envelope of a nonrigid...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
It was a conclusion of this detailed study of the practicality of using airships for carrying passen...
The new method for making computations in connection with the study of rigid airships, which was use...
In this report it is shown that determining the instantaneous angle of pitch, the acceleration of th...
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
This report describes the new method for making computations in connection with the study of rigid a...
The forces and moments acting upon a LTA vehicle are considered in order to develop parameters descr...
Airships used to be the primary passengers' air transportation means before the jet aircraft took ov...
Economic and design characteristics are examined in the design of airplanes and airships
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
The author describes experiments in designing nonrigid airships. A nonrigid airship of 32,000 cubic ...
This report describes the theory of calculating the principal stresses in the envelope of a nonrigid...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
It was a conclusion of this detailed study of the practicality of using airships for carrying passen...
The new method for making computations in connection with the study of rigid airships, which was use...
In this report it is shown that determining the instantaneous angle of pitch, the acceleration of th...
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
This report describes the new method for making computations in connection with the study of rigid a...
The forces and moments acting upon a LTA vehicle are considered in order to develop parameters descr...
Airships used to be the primary passengers' air transportation means before the jet aircraft took ov...
Economic and design characteristics are examined in the design of airplanes and airships
The tests described in this report furnished data on the actual aerodynamic forces, and the resultin...
The author describes experiments in designing nonrigid airships. A nonrigid airship of 32,000 cubic ...
This report describes the theory of calculating the principal stresses in the envelope of a nonrigid...