J. C. Townsend

Pressure data for four analytically defined arrow wings in supersonic flow. [Langley Unitary Plan Wind Tunnel tests]

J. C. Townsend, 1980 .

Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62

William H. Mason, E. J. Landrum, D. S. Miller, 1981 .

Flutter Suppression by Active Control and its Benefits

J. C. Townsend, R. V. Doggett, J. C. Townsend, 1976 .

Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip. [Langley Unitary Plan wind tunnel]

J. C. Townsend, I. K. Collins, J. C. Townsend, 1979 .