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Effects of Specific Types of Surface Roughness on Boundary-Layer Transition

Effects of Specific Types of Surface Roughness on Boundary-Layer Transition

Theoretical and Experimental Data for a Number of NACA 6A-Series Airfoil Sections

Theoretical and experimental data for a number of NACA 6A-series airfoil sections

Aerodynamic Characteristics of a Number of Modified NACA Four-Digit-Series Airfoil Sections

An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number

Theoretical and experimental data for a number of NACA 6A-series airfoil sections

Aerodynamic Characteristics of Several NACA Airfoil Sections at Seven Reynolds Numbers From 0.7 X 10(Exp 6) to 9.0 X 10(Exp 6)

Aerodynamic Characteristics of a Number of Modified NACA Four-Digit-Series Airfoil Sections

Two-dimensional aerodynamic characteristics of 34 miscellaneous airfoil sections

Two-dimensional investigation of five related NACA airfoil sections designed for rotating-wing aircraft

Investigations relating to the extension of laminar flow by means of boundary-layer suction through slots

Investigations Relating to the Extension of Laminar Flow by Means of Boundary-Layer Suction Through Slots

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)

The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Analysis of the effects of boundary-layer control in the take-off and power-off landing performance characteristics of a liaison type of airplane

Exploratory investigation at high and low subsonic Mach numbers of two experimental 6-percent-thick airfoil sections designed to have high maximum lift coefficients

Experimental Investigation of Boundary-Layer Suction Through Slots to Obtain Extensive Laminar Boundary Layers on a 15 Percent-Thick Airfoil Section at High Reynolds Numbers

Experimental investigation of boundary-layer suction through slots to obtain extensive laminar boundary layers on a 15-percent-thick airfoil section at high Reynolds numbers

Experimental Investigation of Laminar-Boundary-Layer Control on an Airfoil Section Equipped With Suction Slots Located at Discontinuities in the Surface Pressure Distribution

Experimental investigation of laminar-boundary-layer control on an airfoil section equipped with suction slots located at discontinuities in the surface pressure distribution

A Rapid Method for Estimating the Separation Point of a Compressible Laminar Boundary Layer

Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)

Airfoil section characteristics at high angles of attack


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