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Continuous, Multielement, Hot-Film Transition Gage (1986)

Holmes, B. ; Mcpherson, J. ; Chapman, J. ; [et al.]

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Publication Date: 2019-07-12

Description: Accurate measurement of location where laminar boundary layer undergoes transition to turbulent one serves many purposes in basic aero-dynamic research and developmental testing. Individual gages must be staggered to prevent formation of turbulence at gages downstream. This arrangement precludes accurate measurements of laminar/turbulent transition regions along streamline. Complete understanding of performance, stability, and control of laminar-flow airplane requires knowledge of transition locations on wing surface, empennage surfaces, fuselage, and nacelles. Visual, acoustic, and electronic methods capable of providing this transition information.

Keywords: MECHANICS

Type: LAR-13319 , NASA Tech Briefs (ISSN 0145-319X); 10; 3; P. 97

Format: text

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