Calculation of Turbine Axial Thrust by Coupled CFD Simulations of the Main Flow Path and Secondary Cavity Flow in an SLI LOX Turbine-Reference-Cited by-同舟云学术

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Calculation of Turbine Axial Thrust by Coupled CFD Simulations of the Main Flow Path and Secondary Cavity Flow in an SLI LOX Turbine

Published:2003-06-26 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Dorney Daniel¹,Marcu Bogdan²,Sargent S²,Tran K²

Affiliation:

1. NASA Marshall Space Flight Center

2. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4919

Reference14 articles.

1. Flow Between Contrarotating Disks

2. Heat transfer measurements in rotating-disc systems Part 2: The rotating cavity with a radial outflow of cooling air

3. An integral method for the calculation of turbulent forced convection in a rotating cavity with radial outflow

4. Graber, D.J., Daniels, W.A., and Johnson, B.V. "Disk Pumping Test: AFWAL-TR-87-2050, 1987.

5. Application of Computational Fluid Dynamics to Turbine Disk Cavities

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1. Design of Axial Force Sensor Based on Equal Strength Beam;Springer Aerospace Technology;2024

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