Add to ORKGThis report is the second of a series giving the results obtained in the 20-foot wind tunnel of the National Advisory Committee for Aeronautics on the interference drag and propulsive efficiency of nacelle-propeller-wing combinations. The first report gave the results of the test of a N.A.C.A. cowled air-cooled engine nacelle located in 21 positions with reference to a thick wing. The present report gives results of tests of a normal engine nacelle with several types of cowling and fairings in four of the positions with reference to the same wing. (author
Report presents the results of an investigation conducted in the Langley propeller research tunnel t...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
Negative thrust and torque data for 2, 3, and 4-blade metal propellers having Clark y and R.A.F. 6 a...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report is the sixth of a series giving wind tunnel tests results on the interference drag and p...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
Report presents the results of an investigation conducted in the NACA 20-foot tunnel to determine th...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
TlLi8 report is the sirth of a 8erit%gz”ningthe rtwults obtained in tlw N.A.C.A. 20-foot wind tunnel...
An extended experimental study has been made in regard to the various refinements in the design of e...
Report presents the results of an investigation conducted in the Langley propeller research tunnel t...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
Negative thrust and torque data for 2, 3, and 4-blade metal propellers having Clark y and R.A.F. 6 a...
This report is the third of a series giving the results obtained in the 20-foot wind tunnel on the i...
This report gives the results in the 20-foot propeller research tunnel of the National Advisory Comm...
This report is the fifth of a series giving the results obtained from wind tunnel tests on the inter...
This report is the sixth of a series giving wind tunnel tests results on the interference drag and p...
A comprehensive investigation has been carried on with full-scale models in the NACA 20-foot wind tu...
Wind-tunnel tests are reported of five 3-blade 10-foot propellers operating in front of a radial and...
Report presents the results of an investigation conducted in the NACA 20-foot tunnel to determine th...
An adjustable blade metal propeller was tested at five different angle settings, forming a series va...
An investigation was conducted in the NACA full-scale wind tunnel to determine the drag and the prop...
The operation of the propeller is analyzed by the use of the distribution of forces along the radius...
TlLi8 report is the sirth of a 8erit%gz”ningthe rtwults obtained in tlw N.A.C.A. 20-foot wind tunnel...
An extended experimental study has been made in regard to the various refinements in the design of e...
Report presents the results of an investigation conducted in the Langley propeller research tunnel t...
Aerodynamic tests were made with four geometrically similar metal propellers of different diameters,...
Negative thrust and torque data for 2, 3, and 4-blade metal propellers having Clark y and R.A.F. 6 a...