Effects of Mach number and specific heat ratio on low-Reynolds-number airfoil flows

M Anyoji, D Numata, H Nagai, K Asai - AIAA journal, 2015 - arc.aiaa.org
The effects of Reynolds number, Mach number, and gas species (air and CO 2) on
aerodynamic characteristics of a thin flat plate and a NACA 0012-34 airfoil were investigated …
被引用次数：79 相关文章
[PDF] researchgate.net

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

M Anyoji, D Numata, H Nagai, K Asai - AIAA JOURNAL, 2015 - researchgate.net
AERODYNAMICS and flow physics at low Reynolds numbers as represented by micro air
vehicles [1], high-altitude, longendurance, unmanned aerial vehicles [2], and insect flight [3] …

Effects of mach number and specific heat ratio on low-reynolds-number airfoil flows

M Anyoji, D Numata, H Nagai, K Asai - AIAA Journal, 2015 - tohoku.elsevierpure.com
The effects of Reynolds number, Mach number, and gas species (air andCO2) on
aerodynamic characteristics of a thin flat plate and a NACA 0012-34 airfoil were investigated …

[引用][C] Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows

M Anyoji, D Numata, H Nagai, K Asai - AIAA Journal, 2015 - cir.nii.ac.jp
Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows | CiNii
Research CiNii 国立情報学研究所 学術情報ナビゲータ[サイニィ] 詳細へ移動 検索フォームへ移動 …

Effects of mach number and specific heat ratio on low-reynolds-number airfoil flows

M Anyoji, D Numata, H Nagai, K Asai - AIAA journal, 2015 - kyushu-u.elsevierpure.com
The effects of Reynolds number, Mach number, and gas species (air andCO2) on
aerodynamic characteristics of a thin flat plate and a NACA 0012-34 airfoil were investigated …

[引用][C] Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows

M Anyoji, D Numata, H Nagai, K Asai - AIAA Journal, 2015 - ui.adsabs.harvard.edu
Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows -
NASA/ADS Now on home page ads icon ads Enable full ADS view NASA/ADS Effects of Mach …