Aerodynamic Pressure and Heating-Rate Distributions in Tile Gaps Around Chine Regions with Pressure Gradients at a Mach Number of 6.6 by National Aeronautics and Space Adm Nasa

Aerodynamic Pressure and Heating-Rate Distributions in Tile Gaps Around Chine Regions with Pressure Gradients at a Mach Number of 6.6

National Aeronautics and Space Adm Nasa

74 pages • missing pub info (editions)

nonfiction science informative slow-paced
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Description

Surface and gap pressures and heating-rate distributions were obtained for simulated Thermal Protection System (TPS) tile arrays on the curved surface test apparatus of the Langley 8-Foot High Temperature Tunnel at Mach 6.6. The results indicated ...

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