In this report it is shown that determining the instantaneous angle of pitch, the acceleration of the gust is as important as its maximum velocity or yaw. Hitherto it has been assumed that the conditions encountered in gusts could be approximately represented by considering the airship to be at an instantaneous angle of yaw or pitch (according to whether the gust is horizontal or vertical), the instantaneous angle being tan to the (-1) power (v/v), where v is the component of the velocity of the gust at right angles to the longitudinal axis of the ship, and v is the speed of the ship. An expression is derived for this instantaneous angle in terms of the speed and certain aerodynamic characteristics of the airship, and of the maximum velocit...
A study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
The purpose of the first two parts of this report is to present in concise format all the formulas r...
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...
Accurate prediction of gust stress being out of the question because of the multiplicity of the free...
This report describes the new method for making computations in connection with the study of rigid a...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
A simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This cri...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
The new method for making computations in connection with the study of rigid airships, which was use...
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A systematic procedure developed for the calculation of the structural response of aircraft flying t...
A study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
The purpose of the first two parts of this report is to present in concise format all the formulas r...
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...
Accurate prediction of gust stress being out of the question because of the multiplicity of the free...
This report describes the new method for making computations in connection with the study of rigid a...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
To furnish data for the design of the fleet airship Shenandoah, a model was made and tested in the 8...
A simple aerodynamic bending moment envelope is derived for conventionally shaped airships. This cri...
The results of the two preceding notes are applied to airships and checked with wind tunnel tests
The problems as to how an airship can best be stabilized and steered and to what stresses it is subj...
The new method for making computations in connection with the study of rigid airships, which was use...
Available information on gust structure, airplane reactions, and pertinent operating statistics has ...
A systematic procedure developed for the calculation of the structural response of aircraft flying t...
A study is made of the longitudinal response of a STOL airplane equipped with a vanecontrolled gust-...
A simple and easily applied method of calculating the dimensions and horsepower necessary for an air...
The purpose of the first two parts of this report is to present in concise format all the formulas r...