Add to ORKGSeveral groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to have lift characteristics at supercritical Mach numbers which are favorable in the sense that the abrupt loss of lift, characteristic of the usual airfoil section at Mach numbers above the critical, is avoided. Aerodynamic characteristics determined from two-dimensional wind-tunnel tests at Mach numbers up to approximately 0.9 are presented for each of the derived airfoils. Comparisons are made between the characteristics of these airfoils and the corresponding characteristics of representative NACA 6-series airfoils
All the supercritical airfoils that have been designed13; to date, to the best knowledge of the auth...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
Refinements in a 10 percent thick supercritical airfoil produced improvements in the overall drag ch...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
The aerodynamic characteristics of an 11 percent thick symmetrical supercritical airfoil were determ...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
Two dimensional wind tunnel test results obtained for supercritical airfoils indicated that substant...
The historical development of NACA airfoils is briefly reviewed. New data are presented that permit ...
The aerodynamic characteristics of several supercritical airfoils interim to the improved 10-percent...
Pressure distributions determined from high-speed wind-tunnel tests are presented for five NACA airf...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
The low speed aerodynamic characteristics of a 14 percent thick supercritical airfoil are documented...
An investigation has been conducted to determine the aerodynamic characteristics of a group of NACA ...
Transonic pressure tunnel and transonic tunnel tests were performed to determine the aerodynamic cha...
All the supercritical airfoils that have been designed13; to date, to the best knowledge of the auth...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
Refinements in a 10 percent thick supercritical airfoil produced improvements in the overall drag ch...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
The aerodynamic characteristics of an 11 percent thick symmetrical supercritical airfoil were determ...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
Several groups of new airfoil sections, designated as the NACA 8-series, are derived analytically to...
Two dimensional wind tunnel test results obtained for supercritical airfoils indicated that substant...
The historical development of NACA airfoils is briefly reviewed. New data are presented that permit ...
The aerodynamic characteristics of several supercritical airfoils interim to the improved 10-percent...
Pressure distributions determined from high-speed wind-tunnel tests are presented for five NACA airf...
Fundamental investigations of compressibility phenomena for airfoils have shown that serious adverse...
The low speed aerodynamic characteristics of a 14 percent thick supercritical airfoil are documented...
An investigation has been conducted to determine the aerodynamic characteristics of a group of NACA ...
Transonic pressure tunnel and transonic tunnel tests were performed to determine the aerodynamic cha...
All the supercritical airfoils that have been designed13; to date, to the best knowledge of the auth...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
Refinements in a 10 percent thick supercritical airfoil produced improvements in the overall drag ch...