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Book Chapter

Linear Stability Theory Applied to Natural and Hybrid Laminar Flow Experiments

  • Schrauf G
  • Horstmann K
Springer Berlin Heidelberg, (2001), 157-163
DOI: 10.1007/978-3-540-45359-8_17
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Abstract

The I'-method is applied to three large-scale experiments performed in the ONERA SIMA wind tunnel and two flight experiments with the ATTAS VFW614 and a Fokker FlOO aircraft. N-factor correlations using incompressible as well compressible linear stability theory obtained for natural and hybrid laminar flow surfaces are discussed.

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Schrauf, G., & Horstmann, K.-H. (2001). Linear Stability Theory Applied to Natural and Hybrid Laminar Flow Experiments. In Aerodynamic Drag Reduction Technologies (pp. 157–163). Springer Berlin Heidelberg. https://doi.org/10.1007/978-3-540-45359-8_17

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