text: NAVWEPS 00-801-80 
  TABLE OF CPNTENTS 
  
  PARASITE DRAG. 
  
  Sources of parasite drag. 
  Parasite drag coefficient.. . . 
  Parasite and induced drag. 
  
  Mi.li$z’.?1 p”‘““ite 
  Airplane efficiency factor 
  Equivalent parasite area 
  
  dr2g CxEciczt 
  
  Effect of configuration. 
  Effect of altitude., 
  Effectofspeed...................................................... 
  
  AIRPLANE TOTAL DRAG.. 
  Drag variation with speed 
  Induced and parasite drag 
  Stall speed 
  Minimum drag 
  Specific performance conditions 
  Compressibility drag rise 
  
  CHAPTER 2. AIRPLANE PERFORMANCE 
  
  REQUIRED THRUST AND POWER 
  
  DEFINITIONS. 
  
  Pan&e 14 ;n&Ced drw 
  __.-__.__._-_- 
  Thrustandpowerrequir~~::::::::::::::::::::::::::::::::::::::::: 
  
  VARIATION OF THRUST AND POWER REQUIRED 
  
  Effect of gross weight. 
  Effect of configuratmn. 
  Effect of altitude. 
  
  AVAILABLE 
  
  THRUST AND POWER 
  PRINCIPLES OF PROPULSION. 
  
  Mass flow, velocity change, momentum change.. 
  Newton’s laws, 
  Wastedpower...............................:..................... 
  Power available. 
  Propulsion efficiency. 
  
  TURBOJET ENGINES 
  
  Operatingcycle.................................................... 
  Function of the components. 
  
  Inlet or diffuser 
  Compressor 
  Combustion chamber 
  Turbine 
  Exhaust nozzle 
  
  Turbojet operating characteristics..  :_
  
  Thrust and power available 
  Effect of velocity 
  Effect of engine speed 
  Specific fuel consumption 
  Effect of altitude 
  Governing apparatus 
  Steady state, acceleration, deceleration 
  Instrumentation 