1. Figure 6 illustrates the thrust producing components of a generic annular nozzle. The nozzle thrust is composed of the thrust developed across the throat TT, the thrust developed by the pressure acting on the cowl surface Tc, the thrust developed by the pressure acting on the centerbody surface Tp and the thrusts acting on the centerbody base area Tpg and the annular base area around the nozzle exit TCE. > 1 A837 10-28-83
2. 8 8 - 8
3. -THEORY I III_ _ _ _ T E S T '1-4845 12 16 83 UNIFORM IVL
4. Figure A-1