Flight tests to determine lift and drag characteristics are discussed. A review is given of the fundamental principles on which the tests are based and on the forces acting on an airplane in the various conditions of steady flight. Glide with and without propeller thrust and the relation between angle of attack and the indicated airspeed for different conditions of steady flight are discussed. The glide test procedure and the problem of the propeller are discussed
"The interrelations established in an earlier report (NACA-TM-921) are used to study the best assump...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Wind tunnel tests of a 15-foot-span model of a two-engine low wing transport airplane were made as a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
Results are given of pressure-distribution measurements made in flight over the right wing cellule a...
The speed, barometric pressure, and number of revolutions of the engine of a seaplane were measured,...
Discussed here are the aerodynamics of a subdivided wing section. The emphasis is upon the increase ...
The analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
The drag and torque of a controllable propeller at various blade-angle settings, and under various d...
This report outlines the flight conditions that are usually critical in determining the design of co...
Comparative flight tests were made with a small parasol monoplane in which the aerodynamic character...
An investigation was made by the NACA wing-flow method to determine the drag, pitching-moment, lift,...
"The interrelations established in an earlier report (NACA-TM-921) are used to study the best assump...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Wind tunnel tests of a 15-foot-span model of a two-engine low wing transport airplane were made as a...
The results of flight tests conducted by the NACA to determine the lift and drag characteristics of ...
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
This investigation was conducted by the National Advisory Committee for Aeronautics at Langley Field...
Flight tests were carried out at the Langley Field laboratory of the NACA, on several airplanes for ...
Results are given of pressure-distribution measurements made in flight over the right wing cellule a...
The speed, barometric pressure, and number of revolutions of the engine of a seaplane were measured,...
Discussed here are the aerodynamics of a subdivided wing section. The emphasis is upon the increase ...
The analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
The drag and torque of a controllable propeller at various blade-angle settings, and under various d...
This report outlines the flight conditions that are usually critical in determining the design of co...
Comparative flight tests were made with a small parasol monoplane in which the aerodynamic character...
An investigation was made by the NACA wing-flow method to determine the drag, pitching-moment, lift,...
"The interrelations established in an earlier report (NACA-TM-921) are used to study the best assump...
This report presents the results of an investigation undertaken to determine the feasibility of maki...
Wind tunnel tests of a 15-foot-span model of a two-engine low wing transport airplane were made as a...