As per the given data in the question,
"\\theta=30^\\circ"
The weight of the plane =100000N
Thrust force on the plane, along the direction of the flight =120000
So, Additional thrust force is "F_{th}"
"\\Rightarrow F_{th}+120000 \\sin 30=100000"
"F_{th}=100000-600000=400000N"
Hence, resist force "R=120000\\cos30=600000\\sqrt{3}N"
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