Add to ORKGIn this mathematical investigation, made in collaboration with Dr. Wilhelm Schmidt, we interpret the temporary change (due to some disturbance) in the quantities which define the position of the airplane while in a flat spin. We further examine the effect of this change, of the means resorted to to produce the disturbance, and thus reveal the expedients available for recovering from a flat spin
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
A discussion is presented of the type of control manipulation and various techniques that may be req...
Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dyna...
This report deals first with the fundamental data required for the investigation. These are chiefly ...
Factors affecting flat spin characteristics of fighter aircraft with horizontal tail surface
Inertia product and inertia moment variation effect on spin entry, developed spin, and spin recovery...
This report deals first with the fundamental data required for the investigation. These are chiefly ...
This report deals with the autorotational characteristics of certain differing wing systems as deter...
The influence of different mathematical and aerodynamic models on computed spin motion was investiga...
Data from wind-tunnel tests on a model of the NY-1 airplane were used in a study of the effect on th...
A preliminarycalculationof an airplanespin-recoverymotionhas been made and the calculationtechniqueh...
With the object of further clarifying the problem of spinning, the equilibrium of the forces and mom...
single-seut jighier airplune wm made for tlu purpose of jinding modijicatti hzt wowk? eliminuie dung...
Systematic flight investigation of the spinning characteristics of various airplanes over a period o...
As part of a general investigation by the NACA of factors that affect the spin, the use of the ailer...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
A discussion is presented of the type of control manipulation and various techniques that may be req...
Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dyna...
This report deals first with the fundamental data required for the investigation. These are chiefly ...
Factors affecting flat spin characteristics of fighter aircraft with horizontal tail surface
Inertia product and inertia moment variation effect on spin entry, developed spin, and spin recovery...
This report deals first with the fundamental data required for the investigation. These are chiefly ...
This report deals with the autorotational characteristics of certain differing wing systems as deter...
The influence of different mathematical and aerodynamic models on computed spin motion was investiga...
Data from wind-tunnel tests on a model of the NY-1 airplane were used in a study of the effect on th...
A preliminarycalculationof an airplanespin-recoverymotionhas been made and the calculationtechniqueh...
With the object of further clarifying the problem of spinning, the equilibrium of the forces and mom...
single-seut jighier airplune wm made for tlu purpose of jinding modijicatti hzt wowk? eliminuie dung...
Systematic flight investigation of the spinning characteristics of various airplanes over a period o...
As part of a general investigation by the NACA of factors that affect the spin, the use of the ailer...
The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high...
A discussion is presented of the type of control manipulation and various techniques that may be req...
Apparatus and techniques were developed for measuring in a low-speed wind tunnel the static and dyna...