Airplane Fuselage-Wing Cross Section Equations and References

AI Thread Summary
The discussion focuses on the equations needed to determine the cross-section between the fuselage and wing of specific aircraft, including the Antonov 140, B-707, Cessna 210, and Cessna Citation. Participants seek references or books that provide these equations, emphasizing the importance of the bulkhead's location in relation to the fuselage and wing. The conversation also highlights the need to derive the exterior part of the cross-section using hand calculations for conic sections, incorporating two points, two slopes, and a curvature point. This technical approach aims to create an accurate representation of the aircraft's cross-section as seen in seating arrangement diagrams. Overall, the thread seeks detailed mathematical guidance for aircraft design analysis.
armin11
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hi guys,
I was wondering what is the equation of cross section between fuselage and wing of the below airplanes:antonov 140 , B-707 , cessna-210 , cessna citation.
Can anyone help?a book or a refrence or whatever you have
 
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Equation of cross section between fuselage and wing? Can you rephrase that? Also, there are more than one model of the citation...
 
There is a bulkhead between the wing and fuselage,a little closer to fuselage from bulkhead is supposed the nedeed region that is almost like the bulkhead I think.like the photo that when airliners want to show how the seating arrangement are in a row in their airplane this cross section is viewed from front of the airplane.we should derive the equation for the exterior part of this cross section using the hand calculating techniques for finding conic sections with two points and two slopes and a user interface point that makes the curvature.
 
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