This report was prepared at the request of the National Advisory Committee for Aeronautics in order to supply a systematic study of the relations between the flight velocity V and its horizontal component V subscript H, in power glides. Curves of V and V subscript H plotted against the inclination of the flight path 0 are given, together with curves which show the maximum values of V subscript H and the corresponding values of 0. Curves are also given showing the effect of small departures from the horizontal in high speed performance testing
Some factors relating to inadvertent speed and Mach number increases in transport operation are disc...
The performance of a glider is determined by means of the velocity polar, which represents the conne...
The reliability of the assumption of a parabolic shape of the polar curve is investigated and found ...
The horizontal tail surfaces of a new airplane usually are proportional so that the curve of moment ...
This report was prepared at the request of the National Advisory Committee for Aeronautics in order ...
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
When an airplane describes a curve it takes a certain time for it to turn from level to inclined pos...
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of nega...
The writer points out briefly the history of the method proposed for the study of steady motion of a...
These experiments were made at the request of the Bureau of Aeronautics, Navy Department, to investi...
War airplanes require not only high speed and the ability to climb rapidly, but also the ability to ...
This report presents general formulas for the determination of all major airplane performance charac...
This investigation was undertaken to determine the relative effects of those factors which may inter...
Lateral-directional dynamic stability derivatives are presented for a O.1-scale model of the XC-142A...
A formula for the computation of the vertical velocity component on all sides of an airplane is dedu...
Some factors relating to inadvertent speed and Mach number increases in transport operation are disc...
The performance of a glider is determined by means of the velocity polar, which represents the conne...
The reliability of the assumption of a parabolic shape of the polar curve is investigated and found ...
The horizontal tail surfaces of a new airplane usually are proportional so that the curve of moment ...
This report was prepared at the request of the National Advisory Committee for Aeronautics in order ...
Flight tests to determine lift and drag characteristics are discussed. A review is given of the fund...
When an airplane describes a curve it takes a certain time for it to turn from level to inclined pos...
Aerodynamic characteristics in pitch of horizontal attitude VTOL aircraft, including effects of nega...
The writer points out briefly the history of the method proposed for the study of steady motion of a...
These experiments were made at the request of the Bureau of Aeronautics, Navy Department, to investi...
War airplanes require not only high speed and the ability to climb rapidly, but also the ability to ...
This report presents general formulas for the determination of all major airplane performance charac...
This investigation was undertaken to determine the relative effects of those factors which may inter...
Lateral-directional dynamic stability derivatives are presented for a O.1-scale model of the XC-142A...
A formula for the computation of the vertical velocity component on all sides of an airplane is dedu...
Some factors relating to inadvertent speed and Mach number increases in transport operation are disc...
The performance of a glider is determined by means of the velocity polar, which represents the conne...
The reliability of the assumption of a parabolic shape of the polar curve is investigated and found ...