Robert R. Graham

Characteristics of a Sealed Internally Balanced Aileron from Tests of a 1/4-Scale Partial-Span Model of the Republic XF-12 Airplane in the Langley 19-Foot Pressure Tunnel

Robert R. Graham, Albert P. Martina, Reino J. Salmi, 1946 .

Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degree Sweptback Wing at Reynolds Numbers to 8,000,000

Robert R. Graham, Reino J. Salmi, D. W. Conner, 1947 .

Summary of Parametric Studies of Flying Crane Helicopters

Robert R. Graham, 1958 .

RESEARCH MEMORANDUM LATERAL-CONTROL INVESTIGATION AT A REYNOLDS NUMBER OF 5,300,000 OF A WING OF ASPECT RATIO 5.8 SWEPTFORWARD 32' AT THE LEADmG EDGE

Robert R. Graham, 1950 .

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

Robert R. Graham, Robert H. Neely, Thomas V. Bollech, 1947 .