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The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine

The Effect of Fuel Consumption on Cylinder Temperatures and Performance of a Cowled Wright J-5 Engine

Comparative flight performance with an NACA Roots supercharger and a turbocentrifugal supercharger

Comparative Performance Obtained With XF7C-1 Airplane Using Several Different Engine Cowlings

The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level

The Comparative Performance of Superchargers

The effect of increased carburetor pressure on engine performance at several compression ratios

The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines

A method for reducing the temperature of exhaust manifolds

The use of large valve overlap in scavenging a supercharged spark-ignition engine using fuel injection

Heat dissipation from a finned cylinder at different fin-plane/air-stream angles

Comparative Performance of a Powerplus Vane-Type Supercharger and an N.A.C.A. Roots-Type Supercharger

Performance of a fuel-injection spark-ignition engine using a hydrogenated safety fuel

Engine performance with a hydrogenated safety fuel

The effect of baffles on the temperature distribution and heat-transfer coefficients of finned cylinders

Cooling characteristics of a 2-row radial engine

Effect of Several Factors on the Cooling of a Radial Engine in Flight

Performance of Air-Cooled Engine Cylinders Using Blower Cooling

The Performance of a DePalma Roots-Type Supercharger

Blower cooling of finned cylinders

Correction of Temperatures of Air-Cooled Engine Cylinders for Variation in Engine and Cooling Conditions

Fuel Consumption of a Carburetor Engine at Various Speeds and Torques

Comparative Performance of Engines Using a Carburetor, Manifold Injection, and Cylinder Injection

Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory

The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder

The Effect of Increased Cooling Surface on Performance of Aircraft-Engine Cylinders as Shown by Tests of the NACA Cylinder

Comparative Cooling of Cylinders of Nonuniform Fin Width With Tight-Fitting Baffles and With Baffles That Provide Constant Flow-Path Areas


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