Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

B Stanford, P Ifju, R Albertani, W Shyy - Progress in Aerospace Sciences, 2008 - Elsevier
Fixed wing micro air vehicles (wingspan between 10 and 15cm) are aerodynamically
challenging due to the low Reynolds number regime (104–105) they operate in. The low …
被引用次数：209 相关文章

[引用][C] Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

B Stanford, P Ifju, R Albertani, W Shyy - Progress in Aerospace Sciences, 2008 - cir.nii.ac.jp
Fixed membrane wings for micro air vehicles: Experimental characterization, numerical
modeling, and tailoring | CiNii Research CiNii 国立情報学研究所 学術情報ナビゲータ[サイニィ] 論文 …
[PDF] psu.edu

[PDF][PDF] Fixed Membrane Wings for Micro Air Vehicles: Experimental Characterization, Numerical Modeling, and Tailoring

B Stanford, P Ifju, R Albertani, W Shyy - Citeseer
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically
challenging due to the low Reynolds number regime (104-105) they operate in. The low …

Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

B Stanford, P Ifju, R Albertani… - Progress in Aerospace …, 2008 - repository.ust.hk
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically
challenging due to the low Reynolds number regime (104-105) they operate in. The low …

Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

B Stanford, P Ifju, R Albertani, W Shyy - Progress in Aerospace Sciences, 2008 - infona.pl
Fixed wing micro air vehicles (wingspan between 10 and 15cm) are aerodynamically
challenging due to the low Reynolds number regime (10 4–10 5) they operate in. The low …
[PDF] academia.edu

[PDF][PDF] Fixed Membrane Wings for Micro Air Vehicles: Experimental Characterization, Numerical Modeling, and Tailoring

B Stanford, P Ifju, R Albertani, W Shyy - academia.edu
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically
challenging due to the low Reynolds number regime (104-105) they operate in. The low …

Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

B Stanford, P Ifju, R Albertani… - Progress in Aerospace …, 2008 - ui.adsabs.harvard.edu
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically
challenging due to the low Reynolds number regime (10 4-10 5) they operate in. The low …
[PDF] academia.edu

[PDF][PDF] Fixed Membrane Wings for Micro Air Vehicles: Experimental Characterization, Numerical Modeling, and Tailoring

B Stanford, P Ifju, R Albertani, W Shyy - academia.edu
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically
challenging due to the low Reynolds number regime (104-105) they operate in. The low …

Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring

B Stanford, P Ifju, R Albertani, W Shyy - Progress in Aerospace Sciences, 2008 - infona.pl
Fixed wing micro air vehicles (wingspan between 10 and 15cm) are aerodynamically
challenging due to the low Reynolds number regime (10 4–10 5) they operate in. The low …

[引用][C] Fixed membrane wings for micro air vehicles: experimental characterization, numerical modeling, and tailoring

B STANFORD - Prog. Aerospace Sci., 2008 - cir.nii.ac.jp
Fixed membrane wings for micro air vehicles : experimental characterization, numerical
modeling, and tailoring | CiNii Research CiNii 国立情報学研究所 学術情報ナビゲータ[サイニィ] …