Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Electro-mechanical actuator

Kenneth E. Schreiner

Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

Scott C. Asbury

A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors

Kenneth H. Goodrich

High-Alpha Research Vehicle (HARV) longitudinal controller

Aaron J. Ostroff

Flight testing the X-36--the test pilot's perspective

Laurence A. Walker

Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane

David E. Reubush

Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

Scott T. Imlay