Add to ORKGMeasurements of surface pressure and wake flow fluctuations were made as part of a transonic wind tunnel investigation into the nature of a supercritical airfoil flow field. Emphasis was on a range of high subsonic Mach numbers and moderate lift coefficients corresponding to the development of drag divergence and buffeting. Fluctuation data were analyzed statistically for intensity, frequency content, and spatial coherence. Variations in these parameters were correlated with changes in the mean airfoil flow field
A combined experimental and computational research program is described for testing and guiding turb...
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Wind tunnel investigation of fluctuating pressures on Centaur model surface at transonic spee
The transonic flow field about a Whitcomb-type supercritical airfoil profile was measured in detail....
A series of experiments was conducted on flow fields about two airfoil models whose sections are sli...
The Langley 8-foot transonic pressure tunnel to determine the wing chordwise pressure distribution f...
The turbulent boundary layer on the wall of a 9 by 7 foot wind tunnel was measured with 12 different...
In order to assess the degree to which the characteristic region of low curvature of the supercritic...
An investigation was conducted in the Langley 8-foot transonic pressure tunnel to determine the effe...
Surface static-pressure and drag data obtained from tests of two slightly modified versions of the o...
This article presents a comprehensive mapping of wall pressure fluctuations over an airfoil under th...
Wind-tunnel tests have been conducted at Mach numbers of 0.85, 0.88, and 0.90 to determine the aerod...
Measurements of surface-pressure fluctuations were made at two locations on the XB-70 airplane for n...
Three high lift systems for a 9.3 percent blunt based, supercritical airfoil were designed, fabricat...
The aerodynamic characteristics of several supercritical airfoils interim to the improved 10-percent...
A combined experimental and computational research program is described for testing and guiding turb...
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Wind tunnel investigation of fluctuating pressures on Centaur model surface at transonic spee
The transonic flow field about a Whitcomb-type supercritical airfoil profile was measured in detail....
A series of experiments was conducted on flow fields about two airfoil models whose sections are sli...
The Langley 8-foot transonic pressure tunnel to determine the wing chordwise pressure distribution f...
The turbulent boundary layer on the wall of a 9 by 7 foot wind tunnel was measured with 12 different...
In order to assess the degree to which the characteristic region of low curvature of the supercritic...
An investigation was conducted in the Langley 8-foot transonic pressure tunnel to determine the effe...
Surface static-pressure and drag data obtained from tests of two slightly modified versions of the o...
This article presents a comprehensive mapping of wall pressure fluctuations over an airfoil under th...
Wind-tunnel tests have been conducted at Mach numbers of 0.85, 0.88, and 0.90 to determine the aerod...
Measurements of surface-pressure fluctuations were made at two locations on the XB-70 airplane for n...
Three high lift systems for a 9.3 percent blunt based, supercritical airfoil were designed, fabricat...
The aerodynamic characteristics of several supercritical airfoils interim to the improved 10-percent...
A combined experimental and computational research program is described for testing and guiding turb...
Turbulent flow field around supersonic space vehicles - identification of separated flow component
Wind tunnel investigation of fluctuating pressures on Centaur model surface at transonic spee