Fuselage Size and kN for known speed and altitude and MTOW
How doth the kN for a set speed change when the size m2 of the fuselage changes though the wingspan (say 14metre) and wing fixed.
Say circular and square and rectangular fuselage section.
Say fuselage diameter 1.5metre, 1.6, 1.7, 1.8, 1.9, 2.0, 2.1. 2.2, 2.3., 2.4, 2.5, 2.6, 2.7, 2.8, 2.9, 3.0, 3.1, 3.2, 3.3, 3.4, 3.5, 3.6, 3.7, 3.8, 3.9, 4.0, 4.1, 4.2metre
Say fuselage nose cone for M0.7-M1.5.
Say set speed 400kts 500kts 600kts 700kts 800kts 900kts 1000kts (M0.7-M1.5)
Say altitudes 500ft 1000ft 2000ft 3000ft 4000ft 5000ft....42000ft
Say MTOW 10,000kg 15,000kg 20,000kg 25,000kg 30,000kg 35,000kg
Experience range 30kN-300kN though what the experience and what the calc.
Say 2.5m square centre fuselage, 14m span, 0.3thick wing, cruise at M0.7 M0.8 M0.9 M1.0 M1.1 M1.2 M1.3 M1.4 M1.5
each altitude
each MTOW
what kN to maintain each speed
Say 3.8m square centre fuselage, 14m span, say 0.3metre thick wing root-tip, cruise at M0.7 M0.8 M0.9 M1.0 M1.1 M1.2 M1.3 M1.4 M1.5
each altitude
each MTOW
what kN to maintain each speed
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