Study on Aerodynamic Characteristics of “Propeller/Wing” System with Overset Mesh Method
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-2689-1_5
Reference14 articles.
1. Fratello G, Favier D, Marescaf C (1991) Experimental and numerical study of the propeller/fixed wing interaction. J Aircraft. https://doi.org/10.2514/3.46036
2. Britcher CP, Landman D, Duvall B et al (2017) An Aeroacoustic study of propellers for small electric propulsion aircraft. In: 23rd AIAA/CEAS aeroacoustics conference. Denver Colorado
3. Catalano FM(2004) On the effects of an installed propeller slipstream on wing aerodynamic characteristics. J Acta Polytechnica.https://doi.org/10.14311/562
4. Jones JR (2017) Development of a very flexible testbed aircraft for the validation of nonlinear aeroelastic codes. PhD thesis, Michigan University
5. Ruiz-Calavera LP, Perdones-Diaz D (2012) CFD based aeroelastic calculation of propeller loads. In: 28th international congress of the aeronautical sciences. Brisbane, Australia
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