Add to ORKGA systematic investigation of the drag associated with cooling air flow in contemporary general aviation engine installations is proposed. Theoretical and experimental methods include a state-of-the-art survey, determination of cooling drag by flight tests, and establishment of relative magnitude and components of cooling drag
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
An extensive survey of current and future airframe construction materials and coolants was conducted...
This paper is one of several dealing with methods intended to reduce the drag of present-day radial ...
A flight-test based research program was performed to investigate the aerodynamics and cooling of a ...
A flight test based research program was performed to investigate the aerodynamics and cooling of a ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76199/1/AIAA-1979-1820-720.pd
A semispan wing and nacelle of a typical general aviation twin-engine aircraft was tested to evaluat...
The pressure recovery of incoming cooling air and the drag associated with engine cooling of a typic...
An extensive series of wind-tunnel tests on a half-scale conventional, nacelle model were made by th...
Tests were made i n the NASA-Ames 40- by 80-Foot Wind Tunnel of a wing semispan with a nacelle (no p...
The state-of-the-art on aerodynamic drag reduction is briefly reviewed. The various elements making ...
The focus of the study is to explore aerodynamic aspects of cooling airflow. As a result of this stu...
An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller ...
This paper examines the aerodynamic design requirements of a cooled cooling air system for a large, ...
The aerodynamic behavior of liquid-cooled aircraft engine cooling installations is reviewed. Design ...
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
An extensive survey of current and future airframe construction materials and coolants was conducted...
This paper is one of several dealing with methods intended to reduce the drag of present-day radial ...
A flight-test based research program was performed to investigate the aerodynamics and cooling of a ...
A flight test based research program was performed to investigate the aerodynamics and cooling of a ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76199/1/AIAA-1979-1820-720.pd
A semispan wing and nacelle of a typical general aviation twin-engine aircraft was tested to evaluat...
The pressure recovery of incoming cooling air and the drag associated with engine cooling of a typic...
An extensive series of wind-tunnel tests on a half-scale conventional, nacelle model were made by th...
Tests were made i n the NASA-Ames 40- by 80-Foot Wind Tunnel of a wing semispan with a nacelle (no p...
The state-of-the-art on aerodynamic drag reduction is briefly reviewed. The various elements making ...
The focus of the study is to explore aerodynamic aspects of cooling airflow. As a result of this stu...
An investigation on the cowling of radial air-cooled engines was conducted in the 20-foot Propeller ...
This paper examines the aerodynamic design requirements of a cooled cooling air system for a large, ...
The aerodynamic behavior of liquid-cooled aircraft engine cooling installations is reviewed. Design ...
This note describes tests of the drag due to a Wright "Whirlwind" (J-5) radial air-cooled engine mou...
An extensive survey of current and future airframe construction materials and coolants was conducted...
This paper is one of several dealing with methods intended to reduce the drag of present-day radial ...