Anyone have experience with gas turbine blade stress analysis?

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SUMMARY

The discussion centers on the stress analysis of gas turbine blades, particularly focusing on aerodynamic forces affecting rotor blades. Participants highlight that while aerodynamic forces are often considered negligible compared to centripetal forces, their impact on blade stiffness and shape changes during operation warrants further investigation. The importance of nonlinear behavior in blade modeling is emphasized, particularly when applying gas loads in a linear analysis. Resources for deeper understanding, including papers and journals, are sought by participants.

PREREQUISITES
  • Understanding of gas turbine blade mechanics
  • Familiarity with rotor and stator blade dynamics
  • Knowledge of linear and nonlinear analysis techniques
  • Basic principles of aerodynamic forces and their calculations
NEXT STEPS
  • Research aerodynamic forces on gas turbine blades in academic journals
  • Study the effects of nonlinear behavior in structural analysis of turbine blades
  • Explore modeling techniques for cantilever beams under distributed loads
  • Investigate the relationship between internal stresses and blade stiffness
USEFUL FOR

Engineers and researchers involved in gas turbine design, aerospace engineers focusing on rotor dynamics, and anyone interested in advanced stress analysis techniques for turbine blades.

AeroStudent
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I'm doing a survey on the topic of "gas turbine blades stress analysis" to see what areas are not focused on in this subject.

I've found that not many people talk about the aerodynamic forces on the blade. Am I missing something, are they included in the calculation or are they too small to consider? Is it worth it to investigate this area?

And does anyone have good resources to study in this area (papers, journals, books,...etc.) , I'm especially interested in the subject of the forces on the blade and how they are distributed.

Thanks in advance.
 
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AeroStudent said:
I've found that not many people talk about the aerodynamic forces on the blade. Am I missing something, are they included in the calculation or are they too small to consider? Is it worth it to investigate this area?
The answer depends on whether you are talking about the rotor or stator blades.

For the rotors, compare the centripetal forces on a typical blade with the aerodynamic forces, and the answer should be fairly obvious. Of course there are no centripetal forces of the stators (often called "guide vanes").
 
Sorry should have specified that I'm talking about rotor blades .

well that's the thing i couldn't find any paper or source that specifies the aerodynamic forces , i know they are very small compared to other stresses but my question is by how much and is it worth it to look into them.
 
It is not just a question of how big the forces are. You also need to consider the change in stiffness of the blade caused by the internal stresses (similar to stretching a guitar string) and the fact that the centripetal forces change as the blade changes shape (because the ##r## in ##mr\omega^2## changes).

If you model a fan blade on a large jet engine as a cantilever beam, and do a linear analysis applying the gas loads as a distributed load along the length of the beam, you will probably get a deflection of the blade tip of the order of 0.5 meters. That is obviously nonsense compared with what happens in real life, and shows how important the nonlinear behavior is.
 

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