1. A t STOL conditions and nominal 10 - 14 degrees angle-of-attack, no large interactions exist between the nose mounted RALS nozzle and wing trailing edge mounted high vector angle thrust nozzles. Airplane stability i s not shifted by operation of the RALS nozzle.
2. Investigation of advanced thrust vectoring exhaust systems for high speed propulsive lift
3. Yip, L. P., and Paulson Jr., J. W. "Effects of Deflected Thrust on the Longitudinal Aerodvnamic Characteristics o f a Close-Coup 1ed ding-Canam Configrarion,' hASA Tcchnical Paper 1090, oateu Uecernber 1977.