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Serial/Series Title: NACA Advanced Confidential Report

Collection: Technical Report Archive and Image Library

Results 21 - 44 of 173

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Blade design data for axial-flow fans and compressors

Blade design data for axial-flow fans and compressors

Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap

Wind-Tunnel Investigation of a Low-Drag Airfoil Section with a Double Slotted Flap

Occurrence of iron oxides on cast-iron engine surfaces after operation

Occurrence of iron oxides on cast-iron engine surfaces after operation

The determination of span load distribution at high speeds by use of high-speed wind-tunnel section data

The determination of span load distribution at high speeds by use of high-speed wind-tunnel section data

A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine I

A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine I

$An electron and x-ray diffraction investigation of surface changes on nitrided-steel piston rings during engine operation in nitrided-steel cylinders barrels$

An electron and x-ray diffraction investigation of surface changes on nitrided-steel piston rings during engine operation in nitrided-steel cylinders barrels

$An electron-diffraction examination of cast-iron piston rings from single-cylinder aircraft engine tests$

An electron-diffraction examination of cast-iron piston rings from single-cylinder aircraft engine tests

Experimental constriction effects in high-speed wind tunnels

Experimental constriction effects in high-speed wind tunnels

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section

Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails

Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails

Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid

Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid

Effects of compressibility on maximum lift coefficients for six propeller airfoils

Effects of compressibility on maximum lift coefficients for six propeller airfoils

Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility

Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility

Flight investigation of the variation of drag coefficient with Mach number for the Bell P-39N-1 airplane

Flight investigation of the variation of drag coefficient with Mach number for the Bell P-39N-1 airplane

Investigation of flow in an axially symmetrical heated jet of air

Investigation of flow in an axially symmetrical heated jet of air

Investigation of the behavior of parallel two-dimensional air jets

Investigation of the behavior of parallel two-dimensional air jets

Investigation of the behavior of parallel two-dimensional air jets

Investigation of the behavior of parallel two-dimensional air jets

Cooling Characteristics of a Pratt and Whitney R-2800 Engine Installed in an NACA Short-Nose High-Inlet-Velocity Cowling

Cooling Characteristics of a Pratt and Whitney R-2800 Engine Installed in an NACA Short-Nose High-Inlet-Velocity Cowling

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Wind-tunnel investigation of ailerons on a low-drag airfoil III : the effect of tabs

Wind-tunnel investigation of ailerons on a low-drag airfoil III : the effect of tabs

Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers

Comparison of calculated and experimental propeller characteristics for four-, six-, and eight-blade single-rotating propellers

The effect of trailing-edge extension flaps on propeller characteristics

The effect of trailing-edge extension flaps on propeller characteristics

Estimation of pressure distributions at subcritical speeds for turrets located on a wing

Estimation of pressure distributions at subcritical speeds for turrets located on a wing

Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage Paint

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