Add to ORKGThe NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented
In order to assess the degree to which the characteristic region of low curvature of the supercritic...
An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...
This report documents the experimental aerodynamic characteristics of a 14 percent thick supercritic...
A concerted effort within the National Aero-nautics and Space Administration (NASA) during the 1960&...
Two supercritical airfoils were developed specifically for application to span distributed loading c...
Two dimensional wind tunnel test results obtained for supercritical airfoils indicated that substant...
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 several supercritical airfoils interim to the improved 10-percent...
The low speed aerodynamic characteristics of a 14 percent thick supercritical airfoil are documented...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
The aerodynamic characteristics of an 11 percent thick symmetrical supercritical airfoil were determ...
An investigation was conducted in the NASA Langley 8-foot transonic pressure tunnel at Mach numbers ...
A 10-percent-thick supercritical airfoil based on an off-design sonic-pressure plateau criterion was...
A lifting airfoil theoretically designed for shockless supercritical flow utilizing a complex hodogr...
In order to assess the degree to which the characteristic region of low curvature of the supercritic...
An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...
This report documents the experimental aerodynamic characteristics of a 14 percent thick supercritic...
A concerted effort within the National Aero-nautics and Space Administration (NASA) during the 1960&...
Two supercritical airfoils were developed specifically for application to span distributed loading c...
Two dimensional wind tunnel test results obtained for supercritical airfoils indicated that substant...
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 several supercritical airfoils interim to the improved 10-percent...
The low speed aerodynamic characteristics of a 14 percent thick supercritical airfoil are documented...
Supercritical airfoils and their applications to wings for various types of aircraft are studied. Th...
The aerodynamic characteristics of an 11 percent thick symmetrical supercritical airfoil were determ...
An investigation was conducted in the NASA Langley 8-foot transonic pressure tunnel at Mach numbers ...
A 10-percent-thick supercritical airfoil based on an off-design sonic-pressure plateau criterion was...
A lifting airfoil theoretically designed for shockless supercritical flow utilizing a complex hodogr...
In order to assess the degree to which the characteristic region of low curvature of the supercritic...
An airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described...
This report documents the experimental aerodynamic characteristics of a 14 percent thick supercritic...