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NACA Technical Reports
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Aircraft compass characteristics
Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel
Analysis of cooling limitations and effect of engine-cooling improvements on level-flight cruising performance of four-engine heavy bomber
An analysis of the factors that determine the periodic twist of an autogiro rotor blade, with a comparison of predicted and measured results
Blower Cooling of Finned Cylinders
Bodies of revolution having minimum drag at high supersonic airspeeds
A Comparison of the Spanwise Loading Calculated by Various Methods With Experimental Loadings Obtained on a 45 Degree Sweptback Wing of Aspect Ratio 8.02 at a Reynolds Number of 4.0 X 10(6)
Critical Compressive Stress for Outstanding Flanges
A description and test results of a spark-ignition and a compression-ignition 2-stroke-cycle engine
Design Charts for Predicting Downwash Angles and Wake Characteristics Behind Plain and Flapped Wings
Effect of moderate air flow on the distribution of fuel sprays after injection cut-off
Effect of NACA Injection Impeller on Mixture Distribution of Double-Row Radial Aircraft Engine
The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight
The effects of fuel and cylinder gas densities on the characteristics of fuel sprays for oil engines
Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails
Flight tests on U.S.S. Los Angeles Part 1: full scale pressure distribution investigation
The Gaseous Explosive Reaction: The Effect of Pressure on the Rate of Propagation of the Reaction Zone and Upon the Rate of Molecular Transformation
Growth of Disturbances in a Flame-Generated Shear Region
Heat transfer to bodies in a high-speed rarified-gas stream
Identification of knock in NACA high-speed photographs of combustion in a spark-ignition engine
Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41
The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines
Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow
The prediction of airfoil characteristics
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