Add to ORKGAn inrestioation ums made in ih N. A. C. A. 7- bw 10+ot m“nd ‘tunnel to determine the aerodynamic se& eharacterie&8 of an A? A. C. A. $3012 airfoil with a tingle main 81.ottedj?ap equipped euccemidy w“th aux-ilia ~ jiap8 of the plain, split, and 810tted types. A te8t kwtal!ation wm U&G?k which an airfoil of Y-foot span was mounted wrh”cal.ly between tb upper and the lower &id @ of the G?0880?teet 8ection 80 fhut two-dime?l&nul $?owwas approximated. & the bm” ~ of maximum lift coej%itvd, hw drag at moderate and high ‘li $ coej%iente, and high drag at high li
The objectives of this study were to verify the predictions of the Eppler Airfoil Design and Analysi...
Section characteridic ~ for uge in WI-W dem”gnare pre-wrded for the N. A. C. A. %7019 airfm”l with p...
Section aerodynamic characteristics of a large-chord N.A.C.A. 23012 airfoil with a slotted deflector...
A test installation was used in which an airfoil of 7-foot span was mounted vertically between the u...
. suMMARY Various auxiliary aixfoi.le having three.d&mnt airfoil sections and wtMrd di$ered char...
An investigation has been made in the N.A.C.A. 7-by lo-foot wind tunnel of a large-chord N.A.C.A. 23...
An investigation has been made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 2...
Report presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel of large-c...
An investigation was made in the NACA 7 by 10-foot wind tunnel of a large-chord NACA 23012 airfoil w...
Report presents the results of wind tunnel tests of the Clark Y, the NACA 23012 and the NACA 23021 a...
An investigation was made in the 7 by 10-foot wind tunnel and in the variable-density wind tunnel of...
An investigation has been made in the N.A.C.A. 7- by 10-foot wind tunnel of a large-chord N.A.C.A. 2...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
This report giaes the results of tests in the N. A. C. A. f+scale and variable-dendy tunnei % of a n...
AN investigation was made of a large-chord NACA 23030 airfoil with a 40- and a 25.66 percent-chord s...
The objectives of this study were to verify the predictions of the Eppler Airfoil Design and Analysi...
Section characteridic ~ for uge in WI-W dem”gnare pre-wrded for the N. A. C. A. %7019 airfm”l with p...
Section aerodynamic characteristics of a large-chord N.A.C.A. 23012 airfoil with a slotted deflector...
A test installation was used in which an airfoil of 7-foot span was mounted vertically between the u...
. suMMARY Various auxiliary aixfoi.le having three.d&mnt airfoil sections and wtMrd di$ered char...
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...
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...
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...
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 7 by 10-foot wind tunnel and in the variable-density wind tunnel of...
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...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
This report giaes the results of tests in the N. A. C. A. f+scale and variable-dendy tunnei % of a n...
AN investigation was made of a large-chord NACA 23030 airfoil with a 40- and a 25.66 percent-chord s...
The objectives of this study were to verify the predictions of the Eppler Airfoil Design and Analysi...
Section characteridic ~ for uge in WI-W dem”gnare pre-wrded for the N. A. C. A. %7019 airfm”l with p...
Section aerodynamic characteristics of a large-chord N.A.C.A. 23012 airfoil with a slotted deflector...