E. Ann Bare

Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle

James R. Burley, George T. Carson, E. Ann Bare, 1987 .

Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47

Francis J. Capone, E. Ann Bare, 1987 .

Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring

E. Ann Bare, David E. Reubush, 1987 .

Investigation of a delta-wing fighter model flow field at transonic speeds

David E. Reubush, E. Ann Bare, Mike Compton, 1987 .