An improved approximate method for calculating lift distributions due to twist

von Sivells, James C.
Veröffentlicht 1951

Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil sections with and without 2° washout

von Sivells, James C.
Veröffentlicht 1947

Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps

von Sivells, James C.
Veröffentlicht 1948

Stalling characteristics and aileron effectiveness of several wing and flap arrangements

von Alexander, S. R.
Veröffentlicht 1945

Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data

von Sivells, James C.
Veröffentlicht 1947

Jet-boundary corrections for complete and semispan swept wings in closed circular wind tunnels

von Sivells, James C.
Veröffentlicht 1951

Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data

von Sivells, James C.
Veröffentlicht 1952

Jet-boundary and plan-form corrections for partial-span models with reflection plane, end plate, or no end plate in a closed circular wind tunnel

von Sivells, James C.
Veröffentlicht 1946

A method of calculating turbulent-boundary-layer growth at hypersonic Mach numbers

von Sivells, James C.
Veröffentlicht 1959

Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data

von Sivells, James C.
Veröffentlicht 1951