AndyErsek85
Airman
Good day ladies and gentlemen
My Name is Andy and I am from Switzerland, 33 years old and I study aircraftingeneering in Zurich (now 5th out of 6 Semesters). In one of my "Subjects" «Aircraft structures and design» I have to make an Analysis project of the Spitfire, including stress calculations and documentation with its Models, aso…
I printed some aircorps-libraryI prints (i read it in an other topic in this Forum) to identify the principal and critical stress Elements. I organized the book "Spitfire - The History" from E.B. Morgan & Ed Shacklady but that didnt help that much Is there any Chance to get some main Details and Pictures about the Aircraft? I mean like measurments (spars, beams, frames etc) and the types of material which where used originally? For that Project i have to analize the structure of the wing tank, identification of critical structure elements (fracture and maintenance critical). Additional to that I should Show the structure design philosophy and introduce what makes the Spitfire so unique.
The Goals of this projekt are stress calculation of the wings and fuselage (bending beams, the Frames and Skin) during manouver.
It would be more than helpful if someone please can help me out with some of the asked details.
Thank you very much
My Name is Andy and I am from Switzerland, 33 years old and I study aircraftingeneering in Zurich (now 5th out of 6 Semesters). In one of my "Subjects" «Aircraft structures and design» I have to make an Analysis project of the Spitfire, including stress calculations and documentation with its Models, aso…
I printed some aircorps-libraryI prints (i read it in an other topic in this Forum) to identify the principal and critical stress Elements. I organized the book "Spitfire - The History" from E.B. Morgan & Ed Shacklady but that didnt help that much Is there any Chance to get some main Details and Pictures about the Aircraft? I mean like measurments (spars, beams, frames etc) and the types of material which where used originally? For that Project i have to analize the structure of the wing tank, identification of critical structure elements (fracture and maintenance critical). Additional to that I should Show the structure design philosophy and introduce what makes the Spitfire so unique.
The Goals of this projekt are stress calculation of the wings and fuselage (bending beams, the Frames and Skin) during manouver.
It would be more than helpful if someone please can help me out with some of the asked details.
Thank you very much