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                  Airplane Structures, part I
                  
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                          Semester 
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                          Lectures +
Exercises 
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                          Subject Designation 
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                          VII 
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                          3 + 1 
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                          18778 
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                    Subject Holder: 
                    
                      Prof.
Dr. Sc.
Ivica
Smojver 
                     
                      
                    Objective: 
                    
                      To familiarize students with
design and basic methods applied in the sizing
of aircraft structural elements. 
                     
                      
                    Description: 
                    
                      - Types of airplanes. Basic
aircraft systems. Concepts of lift surfaces, tail surfaces, propulsion
systems and landing gear.
 
                      - Basic structural elements of a
wing. Concepts and structural solutions of wing structures. Influence
of wing design on basic flying characteristics.
 
                      - Design and sizing of thin walled
beams (main spar).
 
                      - Design and sizing of thin walled
structural elements (wing sections).
 
                      - Design and sizing of compressive
loaded thin walled panels. Critical stress of wing structure – local
and global buckling.
 
                      - Design and sizing of stressed
skin wing.
 
                      - Peculiarities of swept and delta
wing. Concepts and design.
 
                      - Design, sizing and evaluation of
cut-outs. Sizing of reinforced cut-outs. Design and sizing of spars
with cut outs.
 
                      - Basic fuselage structural
elements. Concepts and design solutions. Monocoque and semimonocoque
design. Truss design.
 
                      - Design and sizing of cylindrical
fuselage.
 
                      - Design and sizing of
wing-fuselage joint.
 
                      - Integration of propulsion in the
aircraft structure. Design of intakes.
 
                      - Empennage – concepts and design
solutions.
 
                      - Basic structural element of the
cockpit and cargo area. Concepts and design solutions. Design elements
of fighter airplane cockpit.
 
                      - Zoning. FAR 23 elements
pertinent to the aircraft design.
 
                      - Specifics of composite
aeronautical structures. Examples of typical airplane structures.
 
                     
                      
                    Teaching material: 
                    
                      As provided to students during
lectures 
                     
                      
                    Additional References: 
                    
                      - Niu, M. C. Y.: Airframe
Structural Design, Conmilt Press, 1999.
 
                      - Raymer, D. P.: Aircraft Design:
A Conceptual Approach, AIAA Educational Series, Washington DC, 2002.
 
                      - Glagolev, A.N.; Goljdinov, M.
Ja.; Grigorenko, S.M. : Konstrukcija samoletov, Moskva, Mašinostroenie,
1975.
 
                      - Glagolev, A.N.; Goljdinov, M.
Ja.; Grigorenko, S.M. : Konstrukcija samoletov, Moskva, Mašinostroenie,
1975.
 
                      - Flabel, J.-C.: Practical Stress
Analysis fo Design Engineers, Lake City Publishing Company, 2005.
 
                      - Niu, M. C. Y: Airframe Stress
Analysis and Sizing, Conmilt Press, 1997. 
 
                      - Megson, T.H.G.: Aircraft
Structures for Engineering Students, Elsevier, 2006.
 
                      - Torenbeek, E.; Synthesis of
Subsonic Airplane Design, Kluwer, 1982.
 
                     
                   
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            Administrator        LAST CHANGE: 28.03.2017 | 
           
        
       
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