Funder
State Key Laboratory of Virtual Reality Technology and Systems
Publisher
Springer Science and Business Media LLC
Reference14 articles.
1. Schmidt R (2021) The design of aircraft landing gear. SAE International, Warrendale
2. Huang Y-C (2020) Numerical simulation of the aerodynamic characteristics of a HTHL high-speed demonstrator aircraft. M.S. thesis, School of Aerospace Engineering, Xiamen University
3. Paris AC, Alaverdi O (2005) Nonlinear aerodynamic model extraction from flight-test data for the S-3B viking. J Aircr 42(1):26–32. https://doi.org/10.2514/1.3172
4. Götten F, Havermann M, Braun C, Marino M, Bil C (2020) Wind-tunnel and CFD investigations of UAV landing gears and turrets—improvements in empirical drag estimation. Aerosp Sci Technol 107:106306. https://doi.org/10.1016/j.ast.2020.106306
5. Remillieux MC, Camargo HE, Ravetta PA, Burdisso RA, Ng WF (2008) Novel Kevlar-walled wind tunnel for aeroacoustic testing of a landing gear. AIAA J 46(7):1631–1639. https://doi.org/10.2514/1.33082