Characteristics of the Mars Wind Tunnel at Tohoku University in CO2 Operation Mode-Reference-Cited by-同舟云学术

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Characteristics of the Mars Wind Tunnel at Tohoku University in CO2 Operation Mode

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Anyoji Masayuki¹,Ida Shingo¹,Nose Kei¹,Numata Daijyu¹,Nagai Hiroki¹,Asai Keisuke¹

Affiliation:

1. Tohoku University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1490

Reference13 articles.

1. Evolution of a Mars Airplane Concept for the ARES Mars Scout Mission

2. A Study on Airfoil Design for Future Mars Airplane

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1. A novel design for a dust-induced closed return mars wind tunnel;Planetary and Space Science;2023-10

2. Supersonic Ejector-Driving System under Low Pressure: A Performance Evaluation;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2021

3. Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows;AIAA Journal;2015-06

4. Nonlinear Lift on a Triangular Airfoil in Low-Reynolds-Number Compressible Flow;Journal of Aircraft;2015-05

5. Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel;Journal of Visualization;2014-10-19

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