E. Ann Bare

• Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models
• Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds
• Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
• Investigation of installation effects on twin-engine convergent-divergent nozzles
• Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring
• Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters