The Elusive Onset of Turbulence And the Laminar-Turbulence Interface



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Transcription:

The Elusive Onset of Turbulence And the Laminar-Turbulence Interface

Transition to turbulence Breakdown of organized laminar motion into chaotic flow, or turbulence, is an intriguing phenomenon. The path to turbulence is not unique even in the same flow configuration

Transition to turbulence Breakdown of organized laminar motion into chaotic flow, or turbulence, is an intriguing phenomenon. The path to turbulence is not unique even in the same flow configuration

Characteristics Transition to turbulence enhances mixing enhanced momentum transport

Characteristics Transition to turbulence enhances mixing enhanced momentum transport increases skin friction drag Increases heat transfer rates

Hypersonic flight

Hypersonic flight Columbia: STS 28R (8 th flight) Thermal image from earlier mission (STS 3) shows the effect of turbulent heating. Post-flight analysis of STS-28R discovered unusual heating of the thermal protection system (TPS) during re-entry caused potentially by an early transition to turbulent flow around the vehicle. Columbia STS 107 (28 th flight) Discovery STS 114 First "Return to Flight" Nearly 2.5 years after Columbia Infrared image of Columbia STS 3

Hypersonic flight

Hypersonic flight

Hypersonic flight

Hypersonic flight Columbia: STS 28R (8 th flight) Thermal image from earlier mission (STS 3) shows the effect of turbulent heating. Post-flight analysis of STS-28 discovered unusual heating of the thermal protection system (TPS) during re-entry caused by an early transition to turbulent flow around the vehicle. Columbia STS 107 (28 th flight) Discovery STS 114 First "Return to Flight" Nearly 2.5 years after Columbia Infrared image of Columbia STS 3

Hypersonic flight Columbia: STS 28R (8 th flight) Thermal image from earlier mission (STS 3) shows the effect of turbulent heating. Post-flight analysis of STS-28 discovered unusual heating of the thermal protection system (TPS) during re-entry caused by an early transition to turbulent flow around the vehicle. Columbia STS 107 (28 th flight) Discovery STS 114 First "Return to Flight" Nearly 2.5 years after Columbia

Civil aviation Civil aviation Skin friction is 30-50% of total drag The wings offer highest potential for frictiondrag reduction Laminar flow over 50% of suction surface translates into 5-7% total drag reduction Reduction goals for 2020 Aircraft drag by 10%, wing drag by 20% Jet engines Compressor aerodynamics Flow separation can lead to catastrophic stall Transition to turbulence mitigates stall risk Turbine 20-30% of engine weight 50% of the airfoil chord is transitional flow More aggressive designs for light weight have transition as a key design parameter

Civil aviation Civil aviation Skin friction is 30-50% of total drag The wings offer highest potential for frictiondrag reduction Laminar flow over 50% of suction surface translates into 5-7% total drag reduction Reduction goals for 2020 Aircraft drag by 10%, wing drag by 20% Jet engines Compressor aerodynamics Flow separation can lead to catastrophic stall Transition to turbulence mitigates stall risk Turbine 20-30% of engine weight 50% of the airfoil chord is transitional flow More aggressive designs for light weight have transition as a key design parameter

Challenge Wealth of transition scenarios, with strong sensitivity to flow condition Very large amounts of data; But rare transition events lost to averaging

Opportunity Wealth of transition scenarios, with strong sensitivity to flow condition Very large amounts of data; But rare transition events lost to averaging

Opportunity Wealth of transition scenarios, with strong sensitivity to flow condition - High-fidelity, massively parallel simulations - On the order of 10 9 degrees of freedom - Scalability up to 10 3 10 4 cores Very large amounts of data; But rare transition events lost to averaging

Opportunity Wealth of transition scenarios, with strong sensitivity to flow condition - High-fidelity, massively parallel simulations - On the order of 10 9 degrees of freedom - Scalability up to 10 3 10 4 cores Very large amounts of data; But rare transition events lost to averaging

Opportunity Wealth of transition scenarios, with strong sensitivity to flow condition - High-fidelity, massively parallel simulations - On the order of 10 9 degrees of freedom - Scalability up to 10 3 10 4 cores Very large amounts of data; But rare transition events lost to averaging - Preserve the time and spatial history of the flow - Examine these rare events in full detail

IDIES project An observatory for transition phenomena - First complete temporally and spatially resolved database of laminar-to-turbulence transition - The entire time history from laminar, through transition and into the turbulent regime (~100 TB) - On-demand access to transition events and their evolution - Probe the precursors on transition onset - Provide benchmark for predictive transition modeling

IDIES project An observatory for transition phenomena - First complete temporally and spatially resolved database of laminar-to-turbulence transition - The entire time history from laminar, through transition and into the turbulent regime (~100 TB) - On-demand access to transition events and their evolution - Probe the precursors on transition onset - Provide benchmark for predictive transition modeling

IDIES project An observatory for transition phenomena - First complete temporally and spatially resolved database of laminar-to-turbulence transition - The entire time history from laminar, through transition and into the turbulent regime (~100 TB) - On-demand access to transition events and their evolution - Probe the precursors on transition onset - Provide benchmark for predictive transition modeling

IDIES project An observatory for transition phenomena - First complete temporally and spatially resolved database of laminar-to-turbulence transition - The entire time history from laminar, through transition and into the turbulent regime (~100 TB) - On-demand access to transition events and their evolution - Probe the precursors on transition onset - Provide benchmark for predictive transition modeling

IDIES project An observatory for transition phenomena - First complete temporally and spatially resolved database of laminar-to-turbulence transition - The entire time history from laminar, through transition and into the turbulent regime (~100 TB) - On-demand access to transition events and their evolution - Probe the precursors on transition onset - Provide benchmark for predictive transition modeling