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hey had given wings with the cross sectional area of 10m^2 and answer this questions  1a) Describe all the various forces and stresses experienced by the aircraft wing. 1b) Compare how the various stresses, vary on the ground versus in flight.  2) Sketch the stress-strain diagram and indicate the position of the wing on it. Explain. 3) Describe the important material properties of the wing. Explain. 4) Draw and describe the Shear Force Diagram, from the wing root to the wing tip, as shown in the diagram. 5) The ultimate shear stress of the wing material is 20 kPa. Describe how the safety factor varies, from the wing root to the wing tip. 6) Draw and describe the Bending Moment Diagram, from the wing root to the wing tip, as shown in the diagram. Below picture had list the formula I had learnt so far

hey had given wings with the cross sectional area of 10m^2 and answer this questions  1a) Describe all the various forces and stresses experienced by the aircraft wing. 1b) Compare how the various stresses, vary on the ground versus in flight.  2) Sketch the stress-strain diagram and indicate the position of the wing on it. Explain. 3) Describe the important material properties of the wing. Explain. 4) Draw and describe the Shear Force Diagram, from the wing root to the wing tip, as shown in the diagram. 5) The ultimate shear stress of the wing material is 20 kPa. Describe how the safety factor varies, from the wing root to the wing tip. 6) Draw and describe the Bending Moment Diagram, from the wing root to the wing tip, as shown in the diagram. Below picture had list the formula I had learnt so far

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
Publisher:Kreith, Frank; Manglik, Raj M.
Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.5P: Evaluate the dimensionless groups hcD/k,UD/, and cp/k for water, n-butyl alcohol, mercury, hydrogen,...
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They had given wings with the cross sectional area of 10m^2 and answer this questions 

1a) Describe all the various forces and stresses experienced by the aircraft wing.

1b) Compare how the various stresses, vary on the ground versus in flight. 

2) Sketch the stress-strain diagram and indicate the position of the wing on it. Explain.

3) Describe the important material properties of the wing. Explain.

4) Draw and describe the Shear Force Diagram, from the wing root to the wing tip, as shown in the diagram.

5) The ultimate shear stress of the wing material is
20 kPa. Describe how the safety factor varies, from the wing root to the wing tip.

6) Draw and describe the Bending Moment Diagram, from the wing root to the wing tip, as shown in the diagram.

Below picture had list the formula I had learnt so far

 

ARGIL 4m Lift of 100 kN 26 feet 150% Max Lood 10 feet In Flight Weight of 80 kN FlightBlogger 31 The aircraft wing experiences bending, as shown above. Assume the weight and lift are as illustrated above. Assume the wing has a constant cross-sectional area of 10 m², from wing root to tip.
Transcribed Image Text:ARGIL 4m Lift of 100 kN 26 feet 150% Max Lood 10 feet In Flight Weight of 80 kN FlightBlogger 31 The aircraft wing experiences bending, as shown above. Assume the weight and lift are as illustrated above. Assume the wing has a constant cross-sectional area of 10 m², from wing root to tip.
Hooke's law : F = KAL Force Area Stress = Strain AL 51 FS Lo Ey Ex Young's Modulus = Poisson's ratio = Tu Tall or (units lb/in² or N/m²) 0 = Ee Stress Strain
Transcribed Image Text:Hooke's law : F = KAL Force Area Stress = Strain AL 51 FS Lo Ey Ex Young's Modulus = Poisson's ratio = Tu Tall or (units lb/in² or N/m²) 0 = Ee Stress Strain
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