Aerodynamic Coefficients and Deformation Measurements on Flexible Micro Air Vehicle Wings

By R. Albertani, Bret K. Stanford, J. Hubner, Peter G. Ifju. 2007

165 citations recorded by the source corpus.

Subfields: Aerospace Engineering

View Paper: https://www.semanticscholar.org/paper/dc23f44ad084442a64e6b5304c225205975693c6

How researchers see this paper

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In Aerospace Engineering

1. Zhijin Wang
2. Pinunta Rojratsirikul
3. I. Gursul
4. Wei Shyy
5. Chang-kwon Kang
6. Hikaru Aono

Citations in the corpus

• Flow-induced vibrations of low aspect ratio rectangular membrane wings (2011, background): “It was found that membrane wings can significantly improve longitudinal static stability (Albertani et al., 2007; Stanford et al., 2007), provide more favorable lift-to-drag ratio (Shyy et al., 1999; Lian et al., 2003; Stanford et al., 2008), and delay stall (Lian et al., 2003).”