NAVWEPS 00-807-80  AIRPLANE PERFORMANCE  INLET OR  DIFFUSER  COMPRESSOR  COMBUSTION  TAILPIPE  CHAMBER TURBINE  NOZZLE  2  iiT!  TURBINE WORK  .  E  2  E  Y  it  COMPRESSOR  I  1  c  VOLUME. CU. FT.  Figure 2.6. Turbojet Engines  TURBOJET ENGINE CYCLE  108 