08-06-2012, 01:02 PM
AIRCRAFT STABILITY AND CONTROL
AIRCRAFT STABILITY.pdf (Size: 648.6 KB / Downloads: 5)
POWER EFFECT DUE TO JET PROPULSION
THERE ARE THREE MAJOR CONTRIBUTION
• DIRECT THRUST EFFECT
• DIRECT NORMAL FORCE EFFECT AT AIR DUCT
INTAKE
• INDUCED FLOW AT THE TAIL DUE TO THE
INFLOW TO THE JET BLAST
NOTE: THE ROCKET INSTALLATION WILL ENCOUNTER
FIRST TWO WHILE TURBOJET WILL ENCOUNTER ALL
THREE