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Cavitation Model for Turbopumps in Liquid Rocket Systems

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
56450
Program Year/Program:
2002 / SBIR
Agency Tracking Number:
012459
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Combustion Research and Flow Technology, Inc.
6210 Kellers Church Road Pipersville, PA -
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2002
Title: Cavitation Model for Turbopumps in Liquid Rocket Systems
Agency: NASA
Contract: NAS8-02098
Award Amount: $599,997.00
 

Abstract:

An innovative model for simulating cavitation in liquid rocket turbopumps using cryogenic working fluids is proposed. The formulation is based on a compressible gas-liquid framework that accurately models the acoustics in a multi-phase mixture. This methodology was successfully applied, in our Phase I effort, to simulate cavitating inducer performance in water. Our Phase II effort will extend this formulation to cavitation in cryogenic fluids which exhibit, relative to water, far more complex physics; cryogenic pumps operate at temperatures closer to the critical temperature of the working fluid making thermodynamic effects important. The model will account for the variation in the properties of the fluid as a function of the local fluid temperature that may vary due to energy requirements of vaporization/condensation. It will be incorporated within the commercially marketed code CRUNCH CFD that has a multi-element unstructured framework and is ideally suited for complex turbomachine configurations. This framework will be used as a design support tool to analyze inducer designs and in particular determine the suction specific speed at which head breakdown occurs. The limited reliability of current design tools in cavitating flow regimes makes this innovation a useful tool for turbomachine designers.

Principal Investigator:

Ashvin Hosangadi
Principal Investigator
2152499780
hosangad@craft-tech.com

Business Contact:

Sanford M. Dash
President & Chief Scientist
2152499780
dash@craft-tech.com
Small Business Information at Submission:

Combustion Research and Flow Technology,
174 North Main Street, POB 1150 Dublin, PA 18917

EIN/Tax ID: 232759059
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No