Add to ORKGPressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings of aspect ratios 2 and 4 at Mach numbers of 2.46 and 3.36. The investigation includes some comparison of the effects of Mach number, Reynolds number, and thickening the wing root sections on the loading
suMMARY Pressure distributions on a semispan rectangular wing model having an NACA 0015 airfoil sect...
Wing pressure distribution diagrams for several angles of attack and flap deflections of 0 degrees, ...
Wing was tested with full-span, partial-span, or split flaps deflected 60 Degrees and without flaps....
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
This report presents comprehensive pressure-distribution measurements on four (4) swept-back wings (...
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution ...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Pressure distributions have been obtained in the Langley 8-foot transonic tunnels over a Mach number...
This report presents the results of an exploratory investigation carried out in the Langley 9-inch s...
suMMARY Pressure distributions on a semispan rectangular wing model having an NACA 0015 airfoil sect...
Wing pressure distribution diagrams for several angles of attack and flap deflections of 0 degrees, ...
Wing was tested with full-span, partial-span, or split flaps deflected 60 Degrees and without flaps....
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
This report presents comprehensive pressure-distribution measurements on four (4) swept-back wings (...
An investigation was conducted at a Mach number of 1.90 to determine spanwise pressure distribution ...
Pressure distributions were measured over rectangular wings of aspect ratio 2 and triangular wings o...
Pressure distributions have been obtained in the Langley 8-foot transonic tunnels over a Mach number...
This report presents the results of an exploratory investigation carried out in the Langley 9-inch s...
suMMARY Pressure distributions on a semispan rectangular wing model having an NACA 0015 airfoil sect...
Wing pressure distribution diagrams for several angles of attack and flap deflections of 0 degrees, ...
Wing was tested with full-span, partial-span, or split flaps deflected 60 Degrees and without flaps....