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Evaluation of Aerodynamic Performance of Mars Airplane in Scientific Balloon Experiment

  • Anyoji M
  • Okamoto M
  • Fujita K
  • et al.
Fluid Mechanics Research International Journal (2017) 1(3)
DOI: 10.15406/fmrij.2017.01.00012
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Abstract

… To validate our aerodynamic-design approach using wind tunnels and CFD analyses, we conduct a high-altitude flight test, termed Mars Airplane Balloon Experiment-1 (MABE-1), using …

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APA

Anyoji, M., Okamoto, M., Fujita, K., Nagai, H., & Oyama, A. (2017). Evaluation of Aerodynamic Performance of Mars Airplane in Scientific Balloon Experiment. Fluid Mechanics Research International Journal, 1(3). https://doi.org/10.15406/fmrij.2017.01.00012

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