Add to ORKGThis report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, and U.S.A. 45 airfoils as obtained from tests made in the Variable Density Wind Tunnel. The results are given at both low and high Reynolds numbers to show scale effect and to provide data for use in airplane design.NACA TN no. 367."February, 1931."Includes bibliographical references.This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, and U.S.A. 45 airfoils as obtained from tests made in the Variable Density Wind Tunnel. The results are given at both low and high Reynolds numbers to show scale effect and to provide data for use in airplane design.Mode of access: Internet
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
At the request of the Materiel Division of the Army Air Corps, seven tapered wings having sections b...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
The experimental and calculated aerodynamic characteristics of 22 tapered wings are compared, using ...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The effects of compressibility on the lift, pressure, pitching-moment, and load characteristics of a...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
The maximum lift coefficient for the airplane is compared with that obtained for the Gottingen 387 a...
Two-dimensional tests of eight 6-percent-thick symmetrical airfoils of the supersonic and subsonic t...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
At the request of the Materiel Division of the Army Air Corps, seven tapered wings having sections b...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 393, a...
The experimental and calculated aerodynamic characteristics of 22 tapered wings are compared, using ...
The aerodynamic characteristics of a large number of miscellaneous airfoils tested in the variable-d...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The effects of compressibility on the lift, pressure, pitching-moment, and load characteristics of a...
The effect of scale and turbulence on the lift and drag of five airfoils the NACA 0006, the NACA 002...
An investigation of a large group of related airfoils was made in the NACA variable-density wind tun...
The maximum lift coefficient for the airplane is compared with that obtained for the Gottingen 387 a...
Two-dimensional tests of eight 6-percent-thick symmetrical airfoils of the supersonic and subsonic t...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
The aerodynamic characteristics of 34 miscellaneous airfoils tested in the Langley two-dimensional l...
This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 ...
At the request of the Materiel Division of the Army Air Corps, seven tapered wings having sections b...
Lift, drag, and moment measurements were taken at low Reynolds numbers for four airfoils with traili...