Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows-Reference-Cited by-同舟云学术

Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows

Published:2015-06 Issue:6 Volume:53 Page:1640-1654
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Anyoji Masayuki¹,Numata Daiju²,Nagai Hiroki²,Asai Keisuke²

Affiliation:

1. Department of Space Flight System, Japan Aerospace Exploration Agency, 252-5210 Sagamihara, Japan

2. Department of Aerospace Engineering, Tohoku University, 980-8579 Miyagi, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053468

Reference32 articles.

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2. Design of HALE Aircraft Using Inflatable Wings

3. Flapping Wing Aerodynamics: Progress and Challenges

4. Aerodynamic lift at Reynolds numbers below 7 x 10 exp 4

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