Add to ORKGThis report recounts some of the successful experiments conducted in England and Germany on slotted wings and ailerons. Wind tunnel test results are given and examples of aircraft constructed with these new wing components are described
"The present report is concerned with a series of tests on a model airplane fitted with four types o...
This report presents experiments in which two parts of the wing were arranged so as to form a biplan...
It is to be expected that the advantageous properties, hitherto discovered in many slotted wing sect...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The experiments herein described were made for the purpose of finding whether removing a larger port...
Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotati...
This investigation is an extension of NACA report no. 75 for the purpose of studying the effect of v...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Tests were made in the 7- by 10-foot wind tunnel of the 1/8-scale model of the Brewster F2A airplane...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
A wing equipped with a Zap flap and Zap ailerons was tested on a Fairchild 22 airplane in the full-s...
Tests were made at the Langley two-dimensional low-turbulence pressure tunnel of a mode of the NACA ...
This report contains the results of a series of tests with three wing models. By changing the sectio...
"The present report is concerned with a series of tests on a model airplane fitted with four types o...
This report presents experiments in which two parts of the wing were arranged so as to form a biplan...
It is to be expected that the advantageous properties, hitherto discovered in many slotted wing sect...
This report presents the results of wind-tunnel tests made on three model wings having different siz...
The experiments herein described were made for the purpose of finding whether removing a larger port...
Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotati...
This investigation is an extension of NACA report no. 75 for the purpose of studying the effect of v...
This report gives the results of a recent series of experiments performed on a wing designed for a c...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Tests were made in the 7- by 10-foot wind tunnel of the 1/8-scale model of the Brewster F2A airplane...
Tests were carried out in the small wind tunnel of the Gottingen establishment on a complete model o...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
A wing equipped with a Zap flap and Zap ailerons was tested on a Fairchild 22 airplane in the full-s...
Tests were made at the Langley two-dimensional low-turbulence pressure tunnel of a mode of the NACA ...
This report contains the results of a series of tests with three wing models. By changing the sectio...
"The present report is concerned with a series of tests on a model airplane fitted with four types o...
This report presents experiments in which two parts of the wing were arranged so as to form a biplan...
It is to be expected that the advantageous properties, hitherto discovered in many slotted wing sect...