Analytical procedures and experimental techniques were developed to improve the capability to design advanced high speed propellers. Some results from the propeller lifting line and lifting surface aerodynamic analysis codes are compared with propeller force data, probe data and laser velocimeter data. In general, the code comparisons with data indicate good qualitative agreement. A rotating propeller force balance demonstrated good accuracy and reduced test time by 50 percent. Results from three propeller flow visualization techniques are shown which illustrate some of the physical phenomena occurring on these propellers
Low-speed wind-tunnel performance tests of two advanced propellers have been completed at the NASA L...
Advanced high-speed propellers offer large performance improvements for aircraft that cruise in the ...
Studies of several General Aviation aircraft indicated that the application of advanced technologies...
The performance of lower speed, 5 foot diameter model general aviation propellers, was tested in the...
Several advanced aerodynamic and acoustic concepts were investigated in recent wind tunnel tests per...
Four high speed propeller models were designed and tested in an 8x6 foot wind tunnel in order to eva...
Low speed wind tunnel performance tests of two advanced propellers were completed. The 62.2 cm diame...
The low-speed aerodynamic performance characteristics of two advanced counterrotation pusher-propell...
A preliminary design tool for advanced propellers was developed combining a fast vortex lattice aero...
The torsional deflection of the blades of three full-scale duralumin propellers operating under vari...
Modern high speed propeller (advanced turboprop) aircraft are expected to operate on 50 to 60 percen...
This report tries to give a comprehensive survey of the most important propeller problems such as th...
The relative efficiencies of various engine-propeller combinations were the subject of a study that ...
The increased emphasis on fuel conservation in the world has stimulated a series of studies of both ...
Results are reported of a NASA sponsored analytical investigation into the merits of advanced counte...
Low-speed wind-tunnel performance tests of two advanced propellers have been completed at the NASA L...
Advanced high-speed propellers offer large performance improvements for aircraft that cruise in the ...
Studies of several General Aviation aircraft indicated that the application of advanced technologies...
The performance of lower speed, 5 foot diameter model general aviation propellers, was tested in the...
Several advanced aerodynamic and acoustic concepts were investigated in recent wind tunnel tests per...
Four high speed propeller models were designed and tested in an 8x6 foot wind tunnel in order to eva...
Low speed wind tunnel performance tests of two advanced propellers were completed. The 62.2 cm diame...
The low-speed aerodynamic performance characteristics of two advanced counterrotation pusher-propell...
A preliminary design tool for advanced propellers was developed combining a fast vortex lattice aero...
The torsional deflection of the blades of three full-scale duralumin propellers operating under vari...
Modern high speed propeller (advanced turboprop) aircraft are expected to operate on 50 to 60 percen...
This report tries to give a comprehensive survey of the most important propeller problems such as th...
The relative efficiencies of various engine-propeller combinations were the subject of a study that ...
The increased emphasis on fuel conservation in the world has stimulated a series of studies of both ...
Results are reported of a NASA sponsored analytical investigation into the merits of advanced counte...
Low-speed wind-tunnel performance tests of two advanced propellers have been completed at the NASA L...
Advanced high-speed propellers offer large performance improvements for aircraft that cruise in the ...
Studies of several General Aviation aircraft indicated that the application of advanced technologies...