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...

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Bibliographic Details
Main Authors: Hidemi Takahashi, Mitsuru Kurita, Hidetoshi Iijima, Monami Sasamori
Format: Article
Language:English
Published: MDPI AG 2018-11-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/8/11/2320