Sloshing Wing Dynamics - 2nd Year Project Overview-Reference-Cited by-同舟云学术

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Sloshing Wing Dynamics - 2nd Year Project Overview

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Gambioli Francesco¹,Chamos Apostolos²,Levenhagen Jens³,Behruzi Philipp⁴,Mastroddi Franco⁵,Malan Arnaud⁶,Longshaw Stephen⁷,Skillen Alex⁷,Cooper Jonathan E.⁸,Gonzalez Leo⁹,Marrone Salvatore¹⁰

Affiliation:

1. Airbus UK

2. EASN-TIS

3. Airbus Defence and Space GmbH

4. ArianeGroup SAS

5. Universita degli Studi di Roma La Sapienza

6. University of Cape Town

7. Science and Technology Facilities Council

8. Bristol University Press and Policy Press

9. Universidad Politecnica de Madrid Biblioteca Aeroespacial

10. Consiglio Nazionale delle Ricerche

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-1341

Reference36 articles.

1. Merten, K. F., and Stephenson, B. H. "Some Dynamic Effects of Fuel Motion in Simplified Model Tip Tanks on Suddenly Excited Bending Oscillations," Tech. Rep. TN-2789, NACA, September 1952.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental analysis of liquid vertical slosh damping at vacuum and atmospheric pressures;Journal of Sound and Vibration;2024-03

2. Numerical Calculation of Slosh Dissipation;Applied Sciences;2022-12-03

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