Add to ORKGAn investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller Research Tunnel at Langley Field. Cooling and drag tests were made with each form of cowling. The propulsive efficiency was found to be practically the same with all forms of cowling
Given here are the results of tests made to determine the effect of fuel consumption on the cylinder...
Wind-tunnel tests were conducted on a model wing-nacelle combination to determine the practicability...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...
This report presents the results of an investigation undertaken in the 20-foot Propeller Research Tu...
An extensive series of wind-tunnel tests on a half-scale conventional, nacelle model were made by th...
At the present time there is considerable demand for improvement in the aerodynamic characteristics ...
An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller ...
The development of new cowlings, applicable to a short-nose radial engine, is described. These cowli...
This report presents the results of an investigation undertaken in the 20-foot Propeller Research Tu...
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
Discussed here are problems with the use of cowlings with radial air cooled engines. An XF7C-1 airpl...
Cooling tests were made of a Northrop A-17A attack airplane successively equipped with a conventiona...
Results are given of drag tests of 4/9-scale model radial air-cooled engine nacelles made as a part ...
An extended experimental study has been made in regard to the various refinements in the design of e...
Measurements were made of the cooling on the fronts of model cylinders in a conventional cowling for...
Given here are the results of tests made to determine the effect of fuel consumption on the cylinder...
Wind-tunnel tests were conducted on a model wing-nacelle combination to determine the practicability...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...
This report presents the results of an investigation undertaken in the 20-foot Propeller Research Tu...
An extensive series of wind-tunnel tests on a half-scale conventional, nacelle model were made by th...
At the present time there is considerable demand for improvement in the aerodynamic characteristics ...
An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller ...
The development of new cowlings, applicable to a short-nose radial engine, is described. These cowli...
This report presents the results of an investigation undertaken in the 20-foot Propeller Research Tu...
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
Discussed here are problems with the use of cowlings with radial air cooled engines. An XF7C-1 airpl...
Cooling tests were made of a Northrop A-17A attack airplane successively equipped with a conventiona...
Results are given of drag tests of 4/9-scale model radial air-cooled engine nacelles made as a part ...
An extended experimental study has been made in regard to the various refinements in the design of e...
Measurements were made of the cooling on the fronts of model cylinders in a conventional cowling for...
Given here are the results of tests made to determine the effect of fuel consumption on the cylinder...
Wind-tunnel tests were conducted on a model wing-nacelle combination to determine the practicability...
Data are presented of the flow conditions in the vicinity of an NACA D sub S -type cowling. Tests we...