These investigations consisted chiefly of measurements of the take-off distance under various starting conditions and with the c.g. in different positions; of the climbing speed as a function of the impact pressure and location of the c.g.; of the longitudinal stability and fore-and-aft controllability and of the determination of the elevator forces and characteristics of the elevator control
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Wind tunnel tests were made of a model wing having an aspect ratio of 3 and a tapered plan form with...
In America and England the ground effect has received much attention for a long time, and whole seri...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The purpose of this investigation was to explore the influence of weights of the controls on the sta...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
At the request of the Air Technical Service Command, U.S. Army Air Forces, a 0.22-scale model of a t...
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
The observation that airplane fabrics, after long use, lose their original strength, caused the Germ...
This paper presents the results of tests of six commonly used airfoils: the CYH, the N-22, the C-72,...
Measurements made during flight with the triple recording device which gives the horizontal and vert...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Wind tunnel tests were made of a model wing having an aspect ratio of 3 and a tapered plan form with...
In America and England the ground effect has received much attention for a long time, and whole seri...
The static longitudinal stability of an airplane with locked elevator is usually determined by analy...
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
The purpose of this investigation was to explore the influence of weights of the controls on the sta...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
At the request of the Air Technical Service Command, U.S. Army Air Forces, a 0.22-scale model of a t...
This report is a listing of the different studies conducted by the Institute in May thru August of 1...
The observation that airplane fabrics, after long use, lose their original strength, caused the Germ...
This paper presents the results of tests of six commonly used airfoils: the CYH, the N-22, the C-72,...
Measurements made during flight with the triple recording device which gives the horizontal and vert...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
Recent accidents, which were the result of structural failure in flight, revealed the necessity of a...
Wind tunnel tests were made of a model wing having an aspect ratio of 3 and a tapered plan form with...
In America and England the ground effect has received much attention for a long time, and whole seri...