This note has been prepared for the National Advisory Committee for Aeronautics. It deals with the model rules relating to aeronautical problems, and shows how the characteristics of one airplane can be determined from those of another airplane of different weight or size, and of similar type. If certain rules for the ratios of the dimensions, the weights and the horsepower are followed, a small low-powered airplane can be used for obtaining information as to performance, stability, controllability and maneuverability of a larger prototype, and contrariwise
This report presents the results of flight tests with three different airplanes using several types ...
T.M. 311 gave a short outline of modern theoretical aerodynamics as applied to light airplane design...
The object of this report is to furnish the designer and builder of small airplanes a simple system ...
This note has been prepared for the National Advisory Committee for Aeronautics. It deals with the m...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial le...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
This report presents examples of different methods of comparing aircraft mathematically. In the exam...
Economic and design characteristics are examined in the design of airplanes and airships
The most essential phenomena of aircraft should be classified according to their origin and then mea...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
This report presents the results of flight tests with three different airplanes using several types ...
T.M. 311 gave a short outline of modern theoretical aerodynamics as applied to light airplane design...
The object of this report is to furnish the designer and builder of small airplanes a simple system ...
This note has been prepared for the National Advisory Committee for Aeronautics. It deals with the m...
This investigation was made for the purpose of determining the characteristics of five full-scale pr...
This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial le...
By comparing airplanes of known strength that have resisted all the usual and even extreme air loads...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
This report presents examples of different methods of comparing aircraft mathematically. In the exam...
Economic and design characteristics are examined in the design of airplanes and airships
The most essential phenomena of aircraft should be classified according to their origin and then mea...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
This report presents the results of flight tests with three different airplanes using several types ...
T.M. 311 gave a short outline of modern theoretical aerodynamics as applied to light airplane design...
The object of this report is to furnish the designer and builder of small airplanes a simple system ...