Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections
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AIRFOILS - NACA 64A310 - CHAR , MOMENTS & ORDINATE↗
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Investigation of NACA 64,2-432 and 64,3-440 Airfoil Sections with Boundary-layer Control and an Analytical Study of Their Possible Applications
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AIRFOILS - NACA 64,2-032 - ORDINATES↗
Effects of Compressibility on the Flow past Thick Airfoil Sections
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AIRFOILS - NACA - CHARACTERISTICS EFFECT OF COMPRE↗
The Effects of Variations in Reynolds Number Between 3.0 x 10 to the Power 6 and 25.0 x 10 to the Power 6 upon the Aerodynamic Characteristics of a Number of NACA 6-series Airfoil Sections
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AIRFOILS - NACA 631-012 - CHAR & ORDINATES↗
A Study of Flow Changes Associated with Airfoil Section Drag Rise at Supercritical Speeds
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AIRFOILS - NACA 641-210 - CHARACTERISTICS LOW-DRAG↗
The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A- series airfoil section
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WIND TUNNEL TESTS - AAL - HIGH-SPEED (3 1/2'X1')↗
Effects of compressibility on maximum lift coefficients for six propeller airfoils
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PRESSURE DISTRIBUTION - AIRFOILS - NACA 16-515↗
Completed Tabulation in the United States of Tests of 24 Airfoils at High Mach Numbers (Derived from Interrupted Work at Guidonia, Italy in the 1.31- by 1.74-Foot High-Speed Tunnel)
Two-dimensional data were obtained in Mach range of from 0.40 to 0.94 and Reynolds Number range of (3.4 - 4.2) X 10 Degrees. Results indicate that thickness ratio is dominating shape parameter at high Mach numbers and that aerodynamic advantages are attainable by using thinnest possible sections. Effects of jet boundaries, Reynolds Number, and Data presented are free from jet-boundary and humidity effects.
AIR FLOW VELOCITY, HIGH - SUBSONIC↗
Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel
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PRESSURE DISTRIBUTION-AIRFOILS NACA 64,2-015(MOD )↗
Aerodynamic Characteristics of a Number of Modified NACA Four-digit-series Airfoil Sections
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AIRFOILS - NACA 0012-64 - CHAR , A C , MOMENTS & O↗
Effects of mean-line loading on the aerodynamic characteristics of some low-drag airfoils
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AIRFOIL SURFACES - ROUGHNESS↗
Variation of Peak Pitching-Moment Coefficients for Six Airfoils as Affected by Compressibility
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AIRFOILS - NACA 16-509 - CHAR & MOMENTS - PROPELLE↗
Low-speed Tests of Five NACA 66-series Airfoils Having Mean Lines Designed to Give High Critical Mach Numbers
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AIRFOILS - NACA 66(215)-416 - CHAR , A C , MOMENTS↗
Theoretical and Experimental Data for a Number of NACA 6a-series Airfoil Sections
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AIRFOILS - NACA 641A212 - CHAR , A C MO↗
Comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade
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PRESSURE DISTRIBUTION - AIRFOILS - NACA 65-810↗
Effects of trailing-edge modifications on pitching moment characteristics of airfoils
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AIRFOILS - TRAILING EDGES↗
Two-Dimensional Wind-Tunnel Investigation of Six Airfoil Sections for the Wing of the Vega XP2V-1 Airplane
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AIRFOILS - LOCKHEED D-12A - CHAR , MOMENTS & ORDIN↗
Tests of NACA 65(216)-420 and 66(218)-420 Airfoils at High Speeds
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REYNOLDS NUMBER↗