Thrust vector control

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

Scott C. Asbury.

Evaluation of four advanced nozzle concepts for short takeoff and landing performance

P. Frank Quinto, Guy T. Kemmerly and John W. Paulson.

A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring

Steven A. Johnson.

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

by Scott T. Imlay.

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

Mary L. Mason and James R. Burley II.

Integrated control using the SOFFT control structure

Nesim Halyo.

HARV ANSER flight test data retrieval and processing procedures

Jessie C. Yeager.

Optimal pitch thrust-vector angle and benefits for all flight regimes

Glenn B. Gilyard, Alexander Bolonkin.

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

Robert J. Foley, Odis C. Pendergraft, Jr.

Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

Richard J. Re and Laurence D. Leavitt.