Aerodynamics Caused by Rolling Rates of a Small-Scale Supersonic Flight Experiment Vehicle with a Cranked-Arrow Main Wing

Aerodynamics Caused by Rolling Rates of a Small-Scale Supersonic Flight Experiment Vehicle with a Cranked-Arrow Main Wing

A small-scale supersonic flight experiment vehicle is being developed at Muroran Institute of Technology as a flying testbed for verification of innovative technologies for high-speed atmospheric flights, which are essential to next-generation aerospace transportation systems. Its baseline configura...

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Bibliographic Details
Main Authors: Kazuhide Mizobata, Koji Shirakata, Atsuya Honda, Keisuke Shiono, Yukiya Ishigami, Akihiro Nishida, Masaaki Miura
Format: Article
Language:English
Published: MDPI AG 2025-06-01
Series:Aerospace
Subjects:
aerodynamic derivatives
cranked-arrow wing
rolling rate
roll damping
adverse yaw
Online Access:https://www.mdpi.com/2226-4310/12/7/572
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