Research on aerodynamics of a wing-in-surface-effect ship by theory and experiment

Pham Xuan Tang, Ngo Tri Thang, Pham Vu Uy, Duong Ngoc Hai
Author affiliations

Authors

  • Pham Xuan Tang Technological Air Force and Air Defense Institute
  • Ngo Tri Thang Technological Air Force and Air Defense Institute
  • Pham Vu Uy Military Center of Science and Technology
  • Duong Ngoc Hai Institute of Mechanics, Vietnamese Academy of Science and Technology

DOI:

https://doi.org/10.15625/0866-7136/29/4/5602

Abstract

The paper presents the results of theoretical and experimental studies of the aerodynamic characteristics of a wing-in-surface-effect ship (WISES), which was made under coordination of the Institute of Mechanics, Vietnamese Academy of Science and Technology. The theoretical researches are carried out by the half analytical method and together by the linear and nonlinear vortex lattice methods. The experiment was conducted by the model on wind tunnel OTl of The Technical Institute of Air Force - Air Defense.

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Published

31-12-2007

How to Cite

[1]
P. X. Tang, N. T. Thang, P. V. Uy and D. N. Hai, Research on aerodynamics of a wing-in-surface-effect ship by theory and experiment, Vietnam J. Mech. 29 (2007) 517–528. DOI: https://doi.org/10.15625/0866-7136/29/4/5602.

Issue

Vol. 29 No. 4 (2007)

Section

Research Article

License

Creative Commons License

This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

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