NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Influence of Turbulence Parameters, Reynolds Number, and Body Shape on Stagnation-Region Heat TransferThe purpose of the present work was threefold: (1) to determine if a free-stream turbulence length scale existed that would cause the greatest augmentation in stagnation-region heat transfer over laminar levels; (2) to investigate the effect of velocity gradient on stagnation-region heat transfer augmentation by free-stream turbulence; and (3) to develop a prediction tool for stagnation heat transfer in the presence of free-stream turbulence. Heat transfer was measured in the stagnation region of four models with elliptical leading edges that had ratios of major to minor axes of 1:1, 1.5:1, 2.25:1, and 3:1. Five turbulence-generating grids were fabricated; four were square mesh, biplane grids made from square bars. The fifth grid was an array of fine parallel wires that were perpendicular to the model spanwise direction. Heat transfer data were taken at Reynolds numbers ranging from 37 000 to 228 000. Turbulence intensities were in the range of 1.1 to 15.9% while the ratio of integral length scale to leading-edge diameter ranged from 0.05 to 0.30. Stagnation-point velocity gradient was varied by nearly 50%. Stagnation-region heat transfer augmentation was found to increase with decreasing length scale but no optimum length scale was found. Heat transfer augmentation due to turbulence was found to be unaffected by the velocity gradient near the leading edge. A correlation was developed that fit heat transfer data for the square-bar grids to within +/- 4%.
Document ID
19950022298
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Vanfossen, G. James
(NASA Lewis Research Center Cleveland, OH, United States)
Simoneau, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Ching, Chan Y.
(Syracuse Univ. NY., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TP-3487
E-8882
NAS 1.60:3487
Report Number: NASA-TP-3487
Report Number: E-8882
Report Number: NAS 1.60:3487
Accession Number
95N28719
Funding Number(s)
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available