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"NASA Technical Reports Server (NTRS) 19860017742: Incompressible Boundary-layer Stability Analysis Of LFC Experimental Data For Sub-critical Mach Numbers. M.S. Thesis" and the language of the book is English.


“NASA Technical Reports Server (NTRS) 19860017742: Incompressible Boundary-layer Stability Analysis Of LFC Experimental Data For Sub-critical Mach Numbers. M.S. Thesis” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19860017742: Incompressible Boundary-layer Stability Analysis Of LFC Experimental Data For Sub-critical Mach Numbers. M.S. Thesis
  • Author: ➤  
  • Language: English

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  • Internet Archive ID: NASA_NTRS_Archive_19860017742

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An incompressible boundary-layer stability analysis of Laminar Flow Control (LFC) experimental data was completed and the results are presented. This analysis was undertaken for three reasons: to study laminar boundary-layer stability on a modern swept LFC airfoil; to calculate incompressible design limits of linear stability theory as applied to a modern airfoil at high subsonic speeds; and to verify the use of linear stability theory as a design tool. The experimental data were taken from the slotted LFC experiment recently completed in the NASA Langley 8-Foot Transonic Pressure Tunnel. Linear stability theory was applied and the results were compared with transition data to arrive at correlated n-factors. Results of the analysis showed that for the configuration and cases studied, Tollmien-Schlichting (TS) amplification was the dominating disturbance influencing transition. For these cases, incompressible linear stability theory correlated with an n-factor for TS waves of approximately 10 at transition. The n-factor method correlated rather consistently to this value despite a number of non-ideal conditions which indicates the method is useful as a design tool for advanced laminar flow airfoils.

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