Airfoils with their trailing edge cut away are often found on aircraft, as the fins on the hulls of flying boats and the central section of the wings for affording better visibility. It was therefore of some interest to discover the effect of such cutaways on the lift and drag and on the position of the center of pressure. For this purpose, systematic experiments were performed on two different airfoils, a symmetrical airfoil and an airfoil of medium thickness, with successive shortenings of their chords
In naval architecture, it is customary to determine the wetted surface of a ship by means of some fo...
We will here report on the effects of coarsely roughening not only the pressure side but also the su...
The data from previous NACA pressure-distribution investigations of plain flaps and tabs have been a...
The object of this series of experiments was to determine the influence of the relative vertical pos...
The airplane designer often finds it necessary, in meeting the requirements of visibility, to remove...
Report presents the results of an investigation conducted to determine some of the effects of airfoi...
This report presents experiments in which two parts of the wing were arranged so as to form a biplan...
On of the most important characteristics of an airfoil is the rate of change of lift with angle of a...
It is stated that the index value 6000, as found in normal tests of wing sections with a 20 cm chord...
Holographic interferometry data were acquired on an NACA 64A010 airfoil with an oscillating flap. Th...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
An analytical method is presented for predicting lateral-directional aerodynamic characteristics of ...
Three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections were te...
The static and dynamic characteristics of seven helicopter sections and a fixed-wing supercritical a...
An investigation has been made in the NACA 7- by 10-foot wind tunnel of a large chord NACA 23021 air...
In naval architecture, it is customary to determine the wetted surface of a ship by means of some fo...
We will here report on the effects of coarsely roughening not only the pressure side but also the su...
The data from previous NACA pressure-distribution investigations of plain flaps and tabs have been a...
The object of this series of experiments was to determine the influence of the relative vertical pos...
The airplane designer often finds it necessary, in meeting the requirements of visibility, to remove...
Report presents the results of an investigation conducted to determine some of the effects of airfoi...
This report presents experiments in which two parts of the wing were arranged so as to form a biplan...
On of the most important characteristics of an airfoil is the rate of change of lift with angle of a...
It is stated that the index value 6000, as found in normal tests of wing sections with a 20 cm chord...
Holographic interferometry data were acquired on an NACA 64A010 airfoil with an oscillating flap. Th...
This note is the fifth of a series covering an investigation of a number of related airfoils. It pre...
An analytical method is presented for predicting lateral-directional aerodynamic characteristics of ...
Three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections were te...
The static and dynamic characteristics of seven helicopter sections and a fixed-wing supercritical a...
An investigation has been made in the NACA 7- by 10-foot wind tunnel of a large chord NACA 23021 air...
In naval architecture, it is customary to determine the wetted surface of a ship by means of some fo...
We will here report on the effects of coarsely roughening not only the pressure side but also the su...
The data from previous NACA pressure-distribution investigations of plain flaps and tabs have been a...