Startseite Technik Effects of Greitzer’s parameter and throttle valve coefficient on stall-surge transition in single-stage axial compressors
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Effects of Greitzer’s parameter and throttle valve coefficient on stall-surge transition in single-stage axial compressors

  • Naima Meskine , Djamila Seba ORCID logo EMAIL logo , Mohand Kessal und Mohamed Benghanem
Veröffentlicht/Copyright: 5. September 2025
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Abstract

This study focuses on a single-stage compressor, examining the behavior of surge and rotating stall phenomena in detail. Based on Greitzer’s model, the progression of these instabilities was modeled using a set of four dynamical system equations, solved using the fourth-order Runge–Kutta method. The effects of throttle and Greitzer coefficients denoted respectively as K and B, on these instabilities are analyzed and compared. The principal transition conditions between these two phenomena are discussed.


Corresponding author: Djamila Seba, Dynamic of Engines and Vibroacoustic Laboratory, University M’hamed Bougara of Boumerdes, Boumerdes, Algeria; and Department of General Studies, University of Prince Mugrin, Madinah 42241, Saudi Arabia, E-mail:

Nomenclature (SI Units)

τ ˜

Constant dimensionless time step associated with the development of stall cells (%)

A c

Cross-sectional area of the compressor duct (m 2)

A t

Cross-sectional area of the throttle valve pipe (m 2)

B

Greitzer parameter (%)

Cp

Pressure recovery coefficient

G

Dimensional parameter of the geometry (%)

L c

Effective length of the compressor and duct (m)

U

Tangential speed of the Rotor (m/s)

V p

Plenum volume (m 3)

Φ

Coefficient of the mass flow in the compressor (%)

Φ t

Dimensionless pressure rate in the throttle valve (%)

Ψ

Dimensionless pressure rate in the plenum (%)

Ψ c

Dimensionless pressure rate in compressor (%)

Ψ css

Dimensionless rate of the pressure in the permanent case (%)

a

Speed of sound  m / s

ζ

Dimensionless time (%)

Subscript

1

Initial conditions

c

Compressor

p

Plenum

t

Throttle

Acknowledgements

The researchers wish to extend their sincere gratitude to the Deanship of Scientific Research at the Islamic University of Madinah (KSA) for the support provided to the Post-Publishing Program.

  1. Research ethics: Not applicable.

  2. Informed consent: Not applicable.

  3. Author contributions: All authors have accepted responsibility for the entire content of this manuscript and approved its submission.

  4. Use of Large Language Models, AI and Machine Learning Tools: None declared.

  5. Conflict of interest: The authors state no conflict of interest.

  6. Research funding: None declared.

  7. Data availability: Not applicable.

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Received: 2025-02-10
Accepted: 2025-08-05
Published Online: 2025-09-05

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