Add to ORKGThis report describes the development of airplane characteristics since the war and indicates the direction development should take in the immediate future. Some of the major topics include: the behavior of an airplane about its lateral, vertical, and longitudinal axes. Behavior at large angles of attack and landing characteristics are also included
The longitudinal and lateral-directional dynamic-response characteristics of a 35 degree swept-wing ...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
The progress of airplane performance, measured by speed, is recounted in this article
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This survey is intended to give a general approximate idea of the stability and controllability of G...
A survey of some trends in aircraft design was made in an effort to determine the relation between r...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
Some major milestones in the progression of airplane speeds from subsonic to supersonic are traced. ...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
Measured and predicted dynamic response characteristics of a large flexible swept-wing airplane to c...
This report considers as the dominating characteristic, either the load carried, the speed, the radi...
The data presented have no bearing on performance characteristics of airplane, which were considered...
The abolition of military qualifications gives free scope to new technical possibilities in the deve...
The longitudinal and lateral-directional dynamic-response characteristics of a 35 degree swept-wing ...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...
The progress of airplane performance, measured by speed, is recounted in this article
Tests indicated that: 1) C airplanes with two struts are extremely susceptible to aileron maneuvers,...
This survey is intended to give a general approximate idea of the stability and controllability of G...
A survey of some trends in aircraft design was made in an effort to determine the relation between r...
This report covers an investigation of the application of the theory of dynamic longitudinal stabili...
The information obtained from flight tests in 1927-1928 covers chiefly the effect of the structural ...
Some major milestones in the progression of airplane speeds from subsonic to supersonic are traced. ...
It is endeavored in this report to give a full outline of the problem of airplane stability and to c...
Measured and predicted dynamic response characteristics of a large flexible swept-wing airplane to c...
This report considers as the dominating characteristic, either the load carried, the speed, the radi...
The data presented have no bearing on performance characteristics of airplane, which were considered...
The abolition of military qualifications gives free scope to new technical possibilities in the deve...
The longitudinal and lateral-directional dynamic-response characteristics of a 35 degree swept-wing ...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were...