The cooling of a single-row radial air-cooled engine using several cowling arrangements has been studied in the NACA 20-foot wind tunnel. The results show the effect of the propeller and several cowling arrangements on cooling for various values of the indicated horsepower in the climb condition. A table giving comparative performance of the various cowling arrangements is presented. The dependence of temperature on indicated horsepower and pressure drop across the baffles is shown by charts. Other charts show the limiting indicated horsepower against the pressure drop across the engine and the heat dissipated at various values of the indicated horsepower
This report presents the results of tests conducted to determine the effect of different amounts and...
The cooling characteristics of three R-1830-94 engines, two of which were mounted in a test stand an...
In the design of a cowling a certain pressure drop across the cylinders of a radial air-cooled engin...
An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller ...
This report presents the results of an investigation undertaken in the 20-foot Propeller Research Tu...
Wind-tunnel tests were conducted on a model wing-nacelle combination to determine the practicability...
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-...
This report gives the results of the second portion of an investigation in the twenty-foot Propeller...
An extended experimental study has been made in regard to the various refinements in the design of e...
Adjustable cowling flaps, an adjustable-length cowling skirt, and a bottom opening with adjustable f...
At the present time there is considerable demand for improvement in the aerodynamic characteristics ...
Results of flight tests of the performance and cooling characteristics of three NACA D cowlings and ...
This paper is one of several dealing with methods intended to reduce the drag of present-day radial ...
Report presents the results of a comprehensive experimental study carried out at full scale in the N...
Report presents the results of an investigation of full-scale nose-slot cowlings conducted in the NA...
This report presents the results of tests conducted to determine the effect of different amounts and...
The cooling characteristics of three R-1830-94 engines, two of which were mounted in a test stand an...
In the design of a cowling a certain pressure drop across the cylinders of a radial air-cooled engin...
An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller ...
This report presents the results of an investigation undertaken in the 20-foot Propeller Research Tu...
Wind-tunnel tests were conducted on a model wing-nacelle combination to determine the practicability...
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-...
This report gives the results of the second portion of an investigation in the twenty-foot Propeller...
An extended experimental study has been made in regard to the various refinements in the design of e...
Adjustable cowling flaps, an adjustable-length cowling skirt, and a bottom opening with adjustable f...
At the present time there is considerable demand for improvement in the aerodynamic characteristics ...
Results of flight tests of the performance and cooling characteristics of three NACA D cowlings and ...
This paper is one of several dealing with methods intended to reduce the drag of present-day radial ...
Report presents the results of a comprehensive experimental study carried out at full scale in the N...
Report presents the results of an investigation of full-scale nose-slot cowlings conducted in the NA...
This report presents the results of tests conducted to determine the effect of different amounts and...
The cooling characteristics of three R-1830-94 engines, two of which were mounted in a test stand an...
In the design of a cowling a certain pressure drop across the cylinders of a radial air-cooled engin...