Add to ORKGReport presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determine the aerodynamic properties of tapered wings having partial-span flaps for high lift and ordinary ailerons for lateral control. Each of two Clark-y wings, tapered 5:1 and 5:3, was equipped with partial-span split flaps of two lengths and with ordinary ailerons extending from the outboard ends of the flap to the wing tips. Measurements of wing forces and moments and of aileron hinge moments were made for the two conditions of flaps neutral and deflected
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
The investigation was made to determine the effects of full-span and of partial-span split flaps on ...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
This report presents the results of wind tunnel tests to determine the effectiveness of various meth...
An investigation was made to determine the aerodynamic characteristics of tapered and rectangular wi...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
This report covers the sixth of a series of investigations in which various lateral control devices ...
Aerodynamic force tests were made in the N.A.C.A. 7 by 10 foot wind tunnel on a model Clark Y wing w...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Factors derived from wing theory are presented. By means of these factors, the angle of zero lift, t...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
The investigation was made to determine the effects of full-span and of partial-span split flaps on ...
This report covers the twelfth of a series of tests conducted to compare different lateral control d...
This report presents the results of wind tunnel tests to determine the effectiveness of various meth...
An investigation was made to determine the aerodynamic characteristics of tapered and rectangular wi...
A flight investigation was conducted to determine the lateral-control characteristics of retractable...
Tests were made with ordinary flap-type ailerons on two wings with different amounts of taper, one m...
Discussed here are a series of systematic tests being conducted to compare different lateral control...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
This report is the fourth of a series on systematic tests conducted which compares lateral control d...
This report covers the sixth of a series of investigations in which various lateral control devices ...
Aerodynamic force tests were made in the N.A.C.A. 7 by 10 foot wind tunnel on a model Clark Y wing w...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Factors derived from wing theory are presented. By means of these factors, the angle of zero lift, t...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
Three model wings, two with typical slotted ailerons and one with typical frise ailerons, have been ...
The investigation was made to determine the effects of full-span and of partial-span split flaps on ...