This report gives the results in the 20-foot propeller research tunnel of the National Advisory Committee for Aeronautics on the interference drag and propulsive efficiency of a nacelle-propeller combination located in 21 positions with reference to a thick wing. The lift, drag, and propulsive efficiency were obtained at several angles of attack for each of the 21 locations. A net efficiency was derived for determining the over-all effectiveness of each nacelle location. Best results were obtained with the propeller about 25 per cent of the chord directly ahead of the leading edge. A location immediately above or below the wing near the leading edge was very poor
This investigation is part of an extensive experimental study that has been carried out at full scal...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report gives the results of measurements of the lift, drag, and propeller characteristics of se...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the sixth of a series giving wind tunnel tests results on the interference drag and p...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
Report presents the results of an investigation conducted in the NACA 20-foot tunnel to determine th...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
TlLi8 report is the sirth of a 8erit%gz”ningthe rtwults obtained in tlw N.A.C.A. 20-foot wind tunnel...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
This investigation is part of an extensive experimental study that has been carried out at full scal...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report gives the results of measurements of the lift, drag, and propeller characteristics of se...
This report is the second of a series giving the results obtained in the 20-foot wind tunnel of the ...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report is the sixth of a series giving wind tunnel tests results on the interference drag and p...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
Report presents the results of an investigation conducted in the NACA 20-foot tunnel to determine th...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
TlLi8 report is the sirth of a 8erit%gz”ningthe rtwults obtained in tlw N.A.C.A. 20-foot wind tunnel...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
Aerodynamic tests were made of seven full-scale 10-foot-diameter propellers of recent design compris...
This investigation is part of an extensive experimental study that has been carried out at full scal...
Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-coole...
This report gives the results of measurements of the lift, drag, and propeller characteristics of se...