NAVWEPS GO-BOT-BO  STABILITY AND CONTROL  WING.NACELLE,AND  FUSELAGE  MOMENTS AFFECTED BY  SLIPSTREAM  -DYNAMIC PRESSURE  AT TAIL AFFECTED  BY SLIPSTREAM  WING LIFT AFFECTED  BY SLIPSTREAM  FLOW INDUCED BY  JET EXHAUST  DOWNWASH AT TAIL  Figure 4.12. Indirect Power Effects.  263 