Analysis of Structural Characteristics of a Tandem-Wing Layout Vertical Takeoff and Landing UAV
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-3998-1_140
Reference7 articles.
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3. Smith, M., Patil, M., Hodges, D.: CFD-based analysis of nonlinear aeroelastic behavior of high-aspect ratio wings. In: 19th AIAA Applied Aerodynamics Conference, p. 1582 (2001)
4. Kim, K.S., Lee, I., Yoo, J.H., et al.: Efficient numerical aeroelastic analysis of a high-aspect-ratio wing considering geometric nonlinearity. J. Aircr. 47(1), 338–343 (2010)
5. Tang, D., Dowell, E.H.: Limit-cycle hysteresis response for a high-aspect-ratio wing model. J. Aircr. 39(5), 885–888 (2002)
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