Extensive series of experiments have been conducted at the Bureau of Standards to determine the properties of cooling radiator cores manufactured for airplanes and to develop improvements in design. The analysis of the problem on which this work was based, and consequently the experimental method employed, is different from that commonly used. Instead of attempting to test complete radiators, either full size or in model, uniform sections representing different types of core construction have been tested and an analysis of the results made with a view to determining independently the various factors which influence its performance. This report describes referenced method of analysis in predicting the performance of radiators designed for ae...
Tests were made on the 1927 Williams racer in order to determine the effect of the wing radiator on ...
A systematic investigation of the drag associated with cooling air flow in contemporary general avia...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of a large...
Part 1 is to present the results of tests on 56 types of core in a form convenient for use in the st...
Extensive series of experiments have been conducted at the Bureau of Standards to determine the prop...
Part 1 deals with the head resistance of a number of common types of radiator cores at different spe...
Report describes the methods and apparatus developed and used in the extensive experimental research...
This report contains a survey of past radiator research. This report also is intended as a systemati...
This reports combines the wind tunnel results of radiator tests made at the Navy Aerodynamical Labor...
It was a worthwhile task to research methods to lower the cooling drag of radiators. And the success...
A mathematical analysis of radiator design has been made. The volume of the radiator using least tot...
The experiments discussed here were performed to determine whether radiators having similar cooling ...
This report discusses the effects of roughness, smoothness, and cleanness of cooling surfaces on the...
In order to understand the numerical relations between the air velocity, temperature of the cylinder...
We propose to show how to calculate the cooling capacity of all radiators through which the air flow...
Tests were made on the 1927 Williams racer in order to determine the effect of the wing radiator on ...
A systematic investigation of the drag associated with cooling air flow in contemporary general avia...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of a large...
Part 1 is to present the results of tests on 56 types of core in a form convenient for use in the st...
Extensive series of experiments have been conducted at the Bureau of Standards to determine the prop...
Part 1 deals with the head resistance of a number of common types of radiator cores at different spe...
Report describes the methods and apparatus developed and used in the extensive experimental research...
This report contains a survey of past radiator research. This report also is intended as a systemati...
This reports combines the wind tunnel results of radiator tests made at the Navy Aerodynamical Labor...
It was a worthwhile task to research methods to lower the cooling drag of radiators. And the success...
A mathematical analysis of radiator design has been made. The volume of the radiator using least tot...
The experiments discussed here were performed to determine whether radiators having similar cooling ...
This report discusses the effects of roughness, smoothness, and cleanness of cooling surfaces on the...
In order to understand the numerical relations between the air velocity, temperature of the cylinder...
We propose to show how to calculate the cooling capacity of all radiators through which the air flow...
Tests were made on the 1927 Williams racer in order to determine the effect of the wing radiator on ...
A systematic investigation of the drag associated with cooling air flow in contemporary general avia...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of a large...