Wind-tunnel tests of two tapered wings with straight trailing edges and with constant-chord center sections of different spans

von Neely, Robert H.
Veröffentlicht 1943

Experimental and calculated characteristics of several NACA 44-series wings with aspect ratios of 8, 10, and 12 and taper ratios of 2.5 and 3.5

Veröffentlicht 1947

Summary and analysis of horizontal-tail contribution to longitudinal stability of swept-wing airplanes at low speeds

von Neely, Robert H.
Veröffentlicht 1960

Wind-tunnel investigation of an NACA 66-series 16-percent-thick low-drag tapered wing with Fowler and split flaps

von Neely, Robert H.
Veröffentlicht 1946

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

von Sivells, James C.
Veröffentlicht 1947

Effects of wing and nacelle modifications on drag and wake characteristics of a bomber-type airplane model

von Neely, Robert H.
Veröffentlicht 1945