TURBULENT HEATING FROM A COMPRESSIBLE BOUNDARY LAYER WITH PRESSURE GRADIENT.
Technical Report
·
OSTI ID:4751890
- Research Organization:
- Sandia Labs., Livermore, Calif.
- DOE Contract Number:
- AT(29-1)-789
- NSA Number:
- NSA-23-052512
- OSTI ID:
- 4751890
- Report Number(s):
- SCL-RR--69-70
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
BOUNDARY CONDITIONS
BOUNDARY LAYERS
EQUATIONS
FLUID FLOW
FLUID FLOW/heat transfer from boundary-layer turbulent
effects of pressure gradient on
HEAT TRANSFER
HEAT TRANSFER/model for compressible boundary layer
with pressure gradient
LAYERS
N24300* --Engineering--Heat Transfer & Fluid Flow
NUMERICALS
PRESSURE
THICKNESS
TURBULENCE
BOUNDARY LAYERS
EQUATIONS
FLUID FLOW
FLUID FLOW/heat transfer from boundary-layer turbulent
effects of pressure gradient on
HEAT TRANSFER
HEAT TRANSFER/model for compressible boundary layer
with pressure gradient
LAYERS
N24300* --Engineering--Heat Transfer & Fluid Flow
NUMERICALS
PRESSURE
THICKNESS
TURBULENCE