良いPAR効果が許すWIG主翼の形状について [in Japanese] On the Geometry of Main Wing of WIG Permitted for Good PAR Effect [in Japanese]
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This paper is an important supplement of the previous one, titled as "A systematic computation scheme for PAR-WIG cruising design point." The motive is one point—upper limit of aspect ratio of WIG main wing on which sufficient PAR effect can appear at take-off. Previously this fact was described only qualitatively without any FORTRAN computation, and thus aspect ratio of 6.0 was recommended somewhat arbitrarily. The main purpose of this paper is to clarify this point. Accompanying this, some other requirements on geometry of main wing of WIG are obtained.
- Aeronautical and Space Sciences Japan
Aeronautical and Space Sciences Japan 46(532), 289-295, 1998-05
The Japan Society for Aeronautical and Space Sciences