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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