Recent advances in wing-in-ground effect technology

Author:

GALLINGTON R.1,CHAPLIN H.1,KRAUSE F.1,MILLER J.2,PEMBERTON J.3

Affiliation:

1. U.S. Naval Material Command, David W. Taylor Naval Ship and Research Development Center, Bethesda, Md.

2. Logicon, Inc., Bedford, Mass.

3. Scani Valve Corp., San Diego, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 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. Characteristics of Steady Aerodynamics and Aerodynamic Interactions between Wings of a Canard-Configuration WIG;Journal of the Japan Society of Naval Architects and Ocean Engineers;2017

2. Aerodynamic characteristics of NACA 4412 airfoil section with flap in extreme ground effect;International Journal of Naval Architecture and Ocean Engineering;2009-09

3. Static thrust recovery of PAR craft on solid surfaces;Journal of Fluids and Structures;2008-08

4. Wing-in-ground effect vehicles;Progress in Aerospace Sciences;2006-05

5. Causes for discrepancies in ground effect analyses;The Aeronautical Journal;2002-12

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