Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles

Robert Francis Kunz, Jules Washington V. Lindau, Howard J. Gibeling, Jason M. Mulherin, Dennis J. Bieryla, Erica A. Reese

Research output: Chapter in Book/Report/Conference proceedingConference contribution

7 Citations (Scopus)

Abstract

Unsteady, three-dimensional, multiphase Computational Fluid Dynamic (CFD) analyses of several flows of direct relevance to high speed supercavitating vehicles (HSSVs) have been performed. In this paper, we present a brief overview of the CFD formulation employed, and five sets of results including: 1) prescribed motion 3-D maneuvers of a notional HSSV configuration with a propulsion plume, 2) large scale unsteady simulations of natural cavitation over a wedge configuration, 3) simulation of the "gas-on" transient for a ventilated conical cavitator, 4) simulation of the transition from the re-entrant jet to the "twin vortex" regimes behind a vented conical cavitator, and, 5) simulation of a tube launch followed by rocket engine start-up transient. Each of these analyses represents an element of the broad range of physics to be incorporated in a "complete" model of an HSSV system. These simulations were carried out using High Performance Computing (HPC) resources provided under the US Department of Defense High Performance Computing Modernization Program (DoD HPCMP) "Challenge" program, and details of the computational requirements and resources employed in these analyses are discussed.

Original languageEnglish (US)
Title of host publication41st Aerospace Sciences Meeting and Exhibit
StatePublished - 2003
Event41st Aerospace Sciences Meeting and Exhibit 2003 - Reno, NV, United States
Duration: Jan 6 2003Jan 9 2003

Other

Other41st Aerospace Sciences Meeting and Exhibit 2003
CountryUnited States
CityReno, NV
Period1/6/031/9/03

Fingerprint

dynamic analysis
computational fluid dynamics
Dynamic analysis
Computational fluid dynamics
vehicles
high speed
simulation
Rocket engines
Modernization
resources
Cavitation
Propulsion
Vortex flow
Physics
rocket engines
cavitation
maneuvers
resource
propulsion
cavitation flow

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Kunz, R. F., Lindau, J. W. V., Gibeling, H. J., Mulherin, J. M., Bieryla, D. J., & Reese, E. A. (2003). Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles. In 41st Aerospace Sciences Meeting and Exhibit
Kunz, Robert Francis ; Lindau, Jules Washington V. ; Gibeling, Howard J. ; Mulherin, Jason M. ; Bieryla, Dennis J. ; Reese, Erica A. / Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles. 41st Aerospace Sciences Meeting and Exhibit. 2003.
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abstract = "Unsteady, three-dimensional, multiphase Computational Fluid Dynamic (CFD) analyses of several flows of direct relevance to high speed supercavitating vehicles (HSSVs) have been performed. In this paper, we present a brief overview of the CFD formulation employed, and five sets of results including: 1) prescribed motion 3-D maneuvers of a notional HSSV configuration with a propulsion plume, 2) large scale unsteady simulations of natural cavitation over a wedge configuration, 3) simulation of the {"}gas-on{"} transient for a ventilated conical cavitator, 4) simulation of the transition from the re-entrant jet to the {"}twin vortex{"} regimes behind a vented conical cavitator, and, 5) simulation of a tube launch followed by rocket engine start-up transient. Each of these analyses represents an element of the broad range of physics to be incorporated in a {"}complete{"} model of an HSSV system. These simulations were carried out using High Performance Computing (HPC) resources provided under the US Department of Defense High Performance Computing Modernization Program (DoD HPCMP) {"}Challenge{"} program, and details of the computational requirements and resources employed in these analyses are discussed.",
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Kunz, RF, Lindau, JWV, Gibeling, HJ, Mulherin, JM, Bieryla, DJ & Reese, EA 2003, Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles. in 41st Aerospace Sciences Meeting and Exhibit. 41st Aerospace Sciences Meeting and Exhibit 2003, Reno, NV, United States, 1/6/03.

Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles. / Kunz, Robert Francis; Lindau, Jules Washington V.; Gibeling, Howard J.; Mulherin, Jason M.; Bieryla, Dennis J.; Reese, Erica A.

41st Aerospace Sciences Meeting and Exhibit. 2003.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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T1 - Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles

AU - Kunz, Robert Francis

AU - Lindau, Jules Washington V.

AU - Gibeling, Howard J.

AU - Mulherin, Jason M.

AU - Bieryla, Dennis J.

AU - Reese, Erica A.

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N2 - Unsteady, three-dimensional, multiphase Computational Fluid Dynamic (CFD) analyses of several flows of direct relevance to high speed supercavitating vehicles (HSSVs) have been performed. In this paper, we present a brief overview of the CFD formulation employed, and five sets of results including: 1) prescribed motion 3-D maneuvers of a notional HSSV configuration with a propulsion plume, 2) large scale unsteady simulations of natural cavitation over a wedge configuration, 3) simulation of the "gas-on" transient for a ventilated conical cavitator, 4) simulation of the transition from the re-entrant jet to the "twin vortex" regimes behind a vented conical cavitator, and, 5) simulation of a tube launch followed by rocket engine start-up transient. Each of these analyses represents an element of the broad range of physics to be incorporated in a "complete" model of an HSSV system. These simulations were carried out using High Performance Computing (HPC) resources provided under the US Department of Defense High Performance Computing Modernization Program (DoD HPCMP) "Challenge" program, and details of the computational requirements and resources employed in these analyses are discussed.

AB - Unsteady, three-dimensional, multiphase Computational Fluid Dynamic (CFD) analyses of several flows of direct relevance to high speed supercavitating vehicles (HSSVs) have been performed. In this paper, we present a brief overview of the CFD formulation employed, and five sets of results including: 1) prescribed motion 3-D maneuvers of a notional HSSV configuration with a propulsion plume, 2) large scale unsteady simulations of natural cavitation over a wedge configuration, 3) simulation of the "gas-on" transient for a ventilated conical cavitator, 4) simulation of the transition from the re-entrant jet to the "twin vortex" regimes behind a vented conical cavitator, and, 5) simulation of a tube launch followed by rocket engine start-up transient. Each of these analyses represents an element of the broad range of physics to be incorporated in a "complete" model of an HSSV system. These simulations were carried out using High Performance Computing (HPC) resources provided under the US Department of Defense High Performance Computing Modernization Program (DoD HPCMP) "Challenge" program, and details of the computational requirements and resources employed in these analyses are discussed.

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M3 - Conference contribution

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BT - 41st Aerospace Sciences Meeting and Exhibit

ER -

Kunz RF, Lindau JWV, Gibeling HJ, Mulherin JM, Bieryla DJ, Reese EA. Unsteady, three-dimensional multiphase CFD analysis of maneuvering high speed supercavitating vehicles. In 41st Aerospace Sciences Meeting and Exhibit. 2003