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
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
A comparison of predicted and measured aerodynamic characteristics of the original NACA 23012 airfoi...
This report presents the results of an investigation of the aerodynamic characteristics of the NACA ...
An investigation has "been made of the two-dimensional aerodynamic characteristics of three air...
An investigation was made of the aerodynamic effects of reflexing the trailing edge of three commonl...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
The NACA 23012-4 airfoil was investigated for the purpose of increasing lift by means of blowing out...
This investigation is an extension of NACA report no. 75 for the purpose of studying the effect of v...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The NACA 6A-series airfoil sections were designed to eliminate the trailing-edge cusp which is chara...
September 1958Includes bibliographical references (leaves 48-49)A study of the discrepancy in lift b...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
A comparison of predicted and measured aerodynamic characteristics of the original NACA 23012 airfoi...
This report presents the results of an investigation of the aerodynamic characteristics of the NACA ...
An investigation has "been made of the two-dimensional aerodynamic characteristics of three air...
An investigation was made of the aerodynamic effects of reflexing the trailing edge of three commonl...
An analysis has been made of the lift control effectiveness of a 20-percent-chord plain trailing-edg...
The NACA 23012-4 airfoil was investigated for the purpose of increasing lift by means of blowing out...
This investigation is an extension of NACA report no. 75 for the purpose of studying the effect of v...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The NACA 6A-series airfoil sections were designed to eliminate the trailing-edge cusp which is chara...
September 1958Includes bibliographical references (leaves 48-49)A study of the discrepancy in lift b...
Report presenting an investigation in the 7- by 10-foot wind tunnel of the effects of modifications ...
A comparison of predicted and measured aerodynamic characteristics of the original NACA 23012 airfoi...
This report presents the results of an investigation of the aerodynamic characteristics of the NACA ...