Add to ORKGThe forces and moments acting upon a LTA vehicle are considered in order to develop parameters describing planar motion. Similar expressions for HTA vehicles will be given to emphasize the greater complexity of aerodynamic effects when buoyancy effects cannot be neglected. A brief summary is also given of the use of virtual mass coefficients to calculate loads on airships
This report deals with the investigation of the apparent inertia of an airship hull. The exact solut...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
This report describes the new method for making computations in connection with the study of rigid a...
The new method for making computations in connection with the study of rigid airships, which was use...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
A simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This cri...
The research described in this thesis relates to a highly-maneuverable, almost-lighter-than-air vehi...
AbstractAccording of the force and motion characteristics of the high altitude airship, a six-degree...
The apparent inertia of an airship hull is examined. The exact solution of the aerodynamical problem...
The purpose of the first two parts of this report is to present in concise format all the formulas r...
For a first approximation the air flow around the airship hull is assumed to obey the laws of perfec...
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
This report deals with the investigation of the apparent inertia of an airship hull. The exact solut...
This report deals with the investigation of the apparent inertia of an airship hull. The exact solut...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
This report describes the new method for making computations in connection with the study of rigid a...
The new method for making computations in connection with the study of rigid airships, which was use...
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
A simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This cri...
The research described in this thesis relates to a highly-maneuverable, almost-lighter-than-air vehi...
AbstractAccording of the force and motion characteristics of the high altitude airship, a six-degree...
The apparent inertia of an airship hull is examined. The exact solution of the aerodynamical problem...
The purpose of the first two parts of this report is to present in concise format all the formulas r...
For a first approximation the air flow around the airship hull is assumed to obey the laws of perfec...
In the text are derived simple formulae for determining, directly from the data of wind tunnel tests...
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
This report deals with the investigation of the apparent inertia of an airship hull. The exact solut...
This report deals with the investigation of the apparent inertia of an airship hull. The exact solut...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
This report describes the new method for making computations in connection with the study of rigid a...