Tail-wing Flutter Analyses of a Balloon-based Operation Vehicle for Microgravity Experiments
スポンサーリンク
概要
- 論文の詳細を見る
- 2012-11-04
著者
-
MIYAJI Koji
Department of Ocean and Space System Engineering, Yokohama National University
-
Fujita Kazuhisa
Aerospace Research And Development Directorate Japan Aerospace Exploration Agency
-
Miyaji Koji
Department Of Ocean And Space System Engineering Yokohama National University
-
MACHIDA Kentaro
Department of Ocean and Space System Engineering, Yokohama National University
-
SAWAI Shujiro
The Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
関連論文
- Development of Shock Tube for Ground Testing Reentry Aerothermodynamics
- On Accuracy of Prediction of Flutter Boundaries on Unstructured Grids
- Near-Ultraviolet and Visible Spectroscopy of HAYABUSA Spacecraft Re-Entry
- An Overview of JAXA's Ground-Observation Activities for HAYABUSA Reentry
- Trajectory of HAYABUSA Reentry Determined from Multisite TV Observations
- Detection of Acoustic/Infrasonic/Seismic Waves Generated by Hypersonic Re-Entry of the HAYABUSA Capsule and Fragmented Parts of the Spacecraft
- Tail-wing Flutter Analyses of a Balloon-based Operation Vehicle for Microgravity Experiments
- Infrasound/seismic observation of the Hayabusa reentry : Observations and preliminary results
- Tail-wing Flutter Analyses of a Balloon-based Operation Vehicle for Microgravity Experiments