Add to ORKGA test installation was used in which an airfoil of 7-foot span was mounted vertically between the upper and the lower sides of the closed test section so that two-dimensional flow was approximated
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
An investigation was made in the NACA 7 by 10-foot wind tunnel of a large-chord NACA 23012 airfoil w...
An investigation has been made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 2...
An inrestioation ums made in ih N. A. C. A. 7- bw 10+ot m“nd ‘tunnel to determine the aerodynamic se...
An investigation was made in the LMAL 7- by 10-foot wind tunnel of a NACA 23021 airfoil with a doubl...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip ...
Section aerodynamic characteristics of a large-chord N.A.C.A. 23012 airfoil with a slotted deflector...
AN investigation was made of a large-chord NACA 23030 airfoil with a 40- and a 25.66 percent-chord s...
An investigation has been made in the NACA 7- by 10-foot wind tunnel of a large chord NACA 23021 air...
Report presents the results of a pressure-distribution investigation conducted in the Langley Memori...
Section characteristics for use in wing design are presented for the NACA 23012 airfoil with plain a...
An investigation has been made in the N.A.C.A. 7-by lo-foot wind tunnel of a large-chord N.A.C.A. 23...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
An investigation was made in the NACA 7 by 10-foot wind tunnel of a large-chord NACA 23012 airfoil w...
An investigation has been made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 2...
An inrestioation ums made in ih N. A. C. A. 7- bw 10+ot m“nd ‘tunnel to determine the aerodynamic se...
An investigation was made in the LMAL 7- by 10-foot wind tunnel of a NACA 23021 airfoil with a doubl...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
An investigation was made in the NACA 7- by 10-foot wind tunnel to determine the effect of slot-lip ...
Section aerodynamic characteristics of a large-chord N.A.C.A. 23012 airfoil with a slotted deflector...
AN investigation was made of a large-chord NACA 23030 airfoil with a 40- and a 25.66 percent-chord s...
An investigation has been made in the NACA 7- by 10-foot wind tunnel of a large chord NACA 23021 air...
Report presents the results of a pressure-distribution investigation conducted in the Langley Memori...
Section characteristics for use in wing design are presented for the NACA 23012 airfoil with plain a...
An investigation has been made in the N.A.C.A. 7-by lo-foot wind tunnel of a large-chord N.A.C.A. 23...
A large-chord NACA 23012 airfoil was tested. The airfoil extended completely across the test section...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...