Scheda programma d'esame
AEROSPACE STRUCTURES
MARIO ROSARIO CHIARELLI
Academic year2016/17
CourseAEROSPACE ENGINEERING
Code501II
Credits12
PeriodSemester 1 & 2
LanguageEnglish

ModulesAreaTypeHoursTeacher(s)
AEROSPACE STRUCTURES IING-IND/04LEZIONI60
MARIO ROSARIO CHIARELLI unimap
AEROSPACE STRUCTURES IIING-IND/04LEZIONI60
MARIO ROSARIO CHIARELLI unimap
Programma non disponibile nella lingua selezionata
Learning outcomes
Knowledge

The student who successfully completes the course will have the ability to compute the distribution of stress for typical aerospace structures (wing-boxes, fuselages) adopting the elementary theory approach and the forces method;

will be able to demonstrate a solid knowledge of the buckling behavior of compressed structures; will be aware of the energetic approaches to the study of structural problems;

will be aware of the approach to structural problems based on the use of the finite element method.

The evaluation is based only on the verification executed during the examination (oral).

There is not a weighting procedure to establish the final score.

Syllabus

Course Contents

 

( I ) – Basic Structural Analysis – Static (October-December)

 

Introduction to structural mechanics

Notes and exercises on basic elasticity

Beams in bending, shear and torsion

Principles of aerospace structures construction

Bending, shear and torsion of thin-walled tubes

Stresses in multicell tubes

Discrete models of aerospace structures (wing-box, fuselage)

Effects of axial constraint in the aerospace structures

Correction of the elementary theory results

Notes and exercises on matrix method of structural analysis (Force Method and Displacements Method)

 

 

 ( II ) – Analysis of Aerospace Structures – Static (February - April)

 

Notes and exercises on energy methods of structural analysis

Theory of thin plates

Theory of structural instability (buckling of beams, plates and stiffened panels)

Crippling of compressed structures (crippling of beams, plates and stiffened panels)

 

 

( III ) – Introduction to Finite Element Technique (April - May) – NASTRAN-PATRAN codes

 

Basic notes on the FE discretization procedure

Modeling of beam structures (static analyses)

Modeling of plates and stiffened panels (static analyses)

Modeling of typical aircraft structures (static analyses of fuselages and/or wing-boxes)

Introduction to Linear Buckling Analysis (beams, thin plates, stiffened panels)

Introduction to Modal Analysis of structures (beams, thin plates)

Bibliography
  • Aircraft Structures for Engineering Students H.G. Megson, 4th ed.
  • Theory and Analysis of Flight Structures M. Rivello, 1969
  • Spacecraft Structures and Mechanisms P. Sarafin, 1995
Assessment methods

Oral.

During the exam the student must solve some typcal problems relevant to course contents.

At the end of the solution phase (typically 2 or 3 hours), some questions can be asked to clarify the contents of student work.

Notes

The teacher suggests to attend the lessons.

The course contents are very important and often some examples of application are described during the lessons.

The examples often refers to typical exercises of exams.

Updated: 24/05/2016 12:27