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    Unknown
    In:  Other Sources
    Publication Date: 2019-07-12
    Description: Airfoil design for testing in 0.3-m Transonic Cryogenic Tunnel was symmetrical supercritical shape, consistent with flat-bond-plane bonding-and-channeling technology that had been developed. Technique offers greatly increased flexibility in orifice and pressure-channel layout.
    Keywords: FABRICATION TECHNOLOGY
    Type: LAR-13526 , NASA Tech Briefs (ISSN 0145-319X); 11; 5; P. 71
    Format: text
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