William J. Bursnall

Space shuttle payloads

George W. Morgenthaler, William J. Bursnall, 1973 .

The effects of variations in Reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Laurence K. Loftin, William J. Bursnall, 1948 .

Experimental investigation of the pressure distribution about a yawed circular cylinder in the critical Reynolds number range

William J. Bursnall, Lawrence K. Loftin, 1951 .

Experimental investigation of localized regions of laminar-boundary-layer separation

Laurence K. Loftin, W. J. Bursnall, L. K. Loftin, 1951 .

The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Laurence K. Loftin, William J. Bursnall, 1950 .