Interpolation of Turbulent Boundary Layer Profiles Measured in Flight Using Response Surface Methodology
Turbulent boundary layer profiles on the aircraft surface were characterized by pitot-rake measurements conducted in flight experiments at high subsonic Mach number ranges. Due to slight variations in atmospheric air conditions or aircraft attitudes, such as angles of attack and absolute flight spee...
Main Authors: | Hidemi Takahashi, Mitsuru Kurita, Hidetoshi Iijima, Monami Sasamori |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2018-11-01
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Series: | Applied Sciences |
Subjects: | |
Online Access: | https://www.mdpi.com/2076-3417/8/11/2320 |
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