Session 3: Ice Problems

Objective 1: Explain problems and solutions in case of ice conditions
Objective 2: Give an insight in the today applied research on  ice problems  in aeronautical field

 

Explanation:

The teaching materials will utilized to give essential concepts of problem due to ice accretion on an airplane surface and solutions  for it.

Material:

  • Multimedia black board  +  Power Point Like Software
  • Photos  / Videos

Ice on Fuselage

Figure 8 Ice on a model in a wind tunnel

Model of a fuselage

Figure 9 Simulation model for ice problems

Main activities

  • By  utilizing photos and eventually videos the students will learn technology concerning ice accretion on a flying airplane
  • Student will be asked to figures out analogy with similar events in every day live

Maximum duration:

60 minutes

Main question to be asked:

  • What is the impact of ice accretion on air transportation safety?
  • Ask to the students why high altitude clouds are not yet transformed in ice

Developing of Activity

  • Explain to the students which problems ice accretions on airplane could cause
  • Make the students to compare ice problems in a flying airplane with every days similar problems 
  • Make the students to figure out suggestions for solutions of the ice problem 

Results of Activity

  • To explain that ice accretion could cause stall  problems,  loss of controllability,  engine flame out or even engine explosion, failure on flight strumentations
  • To show to the students the different devices to face ice accretion

 

Experiment 2: Bow and arrow

Description

  • Make a student to lunch an arrow with a bow.
  • Ask the student to tell forces and deformations in each part of the system (included) the arm and the hand of the archer.

Bow and Arrow

Figure 16 Bow and arrow

Explanation

In a system like a bow and arrow loads acts as: compression, traction, bending moment, torque moment, etc. Each of them cause on a single system element deformation as: shortening, lengthening, bending, etc...

Results

The aeronautical structures are subject to different kind of loads. So they have to be designed and manufactured so that they would be able to withstand all kind of loads.

Contact coordinator

Dr. Corieri Patricia

von Karman Institute for Fluid Dynamics
Chaussée de Waterloo 72
BE 1640 Rhode-Saint-Genèse

Tel: +32 (0)2 359 96 55
Fax: +32 (0)2 359 96 00

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