A CONCEPTUAL STUDY FOR A NEW WINGED SURFACE EFFECT VEHICLE SYSTEM

Author:

McMASTERS JOHN H.,GREER RICHARD R.

Publisher

Wiley

Subject

Ocean Engineering

Reference10 articles.

1. On the Minimum Induced Drag of Ground-Effect Wings;Ashill;The Aeronautical Quarterly,1970

2. 2. Fink, M. P. and J. L. Lastinger , “Aerodynamic Characteristics of Low-Aspect-Ratio Wings in Close Proximity to the Ground”, NASA TN D-926 (1961).

3. 3. Greer, R. R. , Hydroplane Transport System, U. S. Patent No. 3,635,035 (1972) and Watercraft, U. S. Patent No. 3,768,429 (1973).

4. Size Effects in Conventional Aircraft Design;Cleveland;J. Aircraft,-1970

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

2. BASIC OCEAN VEHICLE ASSESSMENT;Naval Engineers Journal;1976-04

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