AIRCRAFT STABILITY AND CONTROL
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AIRCRAFT STABILITY AND CONTROL


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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
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