Impulsively started incompressible turbulent jet
Hot-film anemometer measurements are presented for the centerline velocity of a suddenly started jet of air. The tip penetration of the jet is shown to be proportional to the square-root of time. A theoretical model is developed that assumes the transient jet can be characterized as a spherical vortex interacting with a steady-state jet. The model demonstrates that the ratio of nozzle radius to jet velocity defines a time constant that uniquely characterizes the behavior and similarity of impulsively started incompressible turbulent jets.
- Research Organization:
- Sandia National Lab. (SNL-CA), Livermore, CA (United States)
- DOE Contract Number:
- AC04-76DP00789
- OSTI ID:
- 5017517
- Report Number(s):
- SAND-80-8617
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
42 ENGINEERING
33 ADVANCED PROPULSION SYSTEMS
INTERNAL COMBUSTION ENGINES
FUEL INJECTION SYSTEMS
MATHEMATICAL MODELS
TURBULENT FLOW
AERODYNAMICS
AIR
EXPERIMENTAL DATA
FLOW RATE
HOT WIRE ANEMOMETERS
JETS
THEORETICAL DATA
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FLUID FLOW
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MEASURING INSTRUMENTS
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420400* - Engineering- Heat Transfer & Fluid Flow
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33 ADVANCED PROPULSION SYSTEMS
INTERNAL COMBUSTION ENGINES
FUEL INJECTION SYSTEMS
MATHEMATICAL MODELS
TURBULENT FLOW
AERODYNAMICS
AIR
EXPERIMENTAL DATA
FLOW RATE
HOT WIRE ANEMOMETERS
JETS
THEORETICAL DATA
ANEMOMETERS
DATA
ENGINES
FLUID FLOW
FLUID MECHANICS
FLUIDS
FUEL SYSTEMS
GASES
HEAT ENGINES
INFORMATION
MEASURING INSTRUMENTS
MECHANICS
NUMERICAL DATA
420400* - Engineering- Heat Transfer & Fluid Flow
330100 - Internal Combustion Engines