The final report consists of an AIAA and an ASME paper. An experimental investigation was conducted to measure skin friction along the chamber walls of supersonic combustors. A direct force measurement device was used to simultaneously measure an axial and transverse component of the small tangential shear force passing over a non-intrusive floating element. Skin friction coefficients between 0.001-0.005 were measured dependent on the facility and measurement location . Analysis of the measurement uncertainties indicate an accuracy to within + or - 10-15% of the streamwise component.... Scramjets, Hypersonics.
Direct Measurements of Skin Friction in Supersonic Combustion Flow Fields
1993
17 pages
Report
Keine Angabe
Englisch
Reciprocation & Rotating Combustion Engines , Fluid Mechanics , Combustors , Skin friction , Accuracy , Chambers , Coefficients , Measurement , Transverse , Uncertainty , Walls , Supersonic combustion , Three dimensional , Turbulent boundary layer , Supersonic combustion ramjet engines , Combustible flow
Direct Measurements of Skin Friction in Supersonic Combustion Flow Fields (92-GT-320)
Online Contents | 1993
|SKIN FRICTION MEASUREMENTS AT SUPERSONIC FLOW VELOCITIES
British Library Conference Proceedings | 2003
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