On the Geometry of Main Wing of WIG Permitted for Good PAR Effect.

• ANDO Shigenori

  徳島文理大学

Bibliographic Information

Other Title

• 良いＰＡＲ効果が許すＷＩＧ主翼の形状について
• ヨイ PAR コウカ ガ ユルス WIG シュヨク ノ ケイジョウ ニ ツイテ

Abstract

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.

Journal

• Aeronautical and Space Sciences Japan

  Aeronautical and Space Sciences Japan 46 (532), 289-295, 1998

  THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Keywords

• PAR Effect
• WIG
• Wing Geometry

Details

• CRID: 1390001204478662912
• NII Article ID: 10002862798
• NII Article ID: 10004069402
• NII Book ID: AN00189072
• DOI: 10.2322/jjsass1969.46.289
• ISSN: 24241369
• ISSN: 00214663
• NDL BIB ID: 4469552
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I4469552
• Web Site: https://www.jstage.jst.go.jp/article/jjsass1969/46/532/46_532_289/_pdf
• Text Lang: ja
• Data Source:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• Abstract License Flag: Disallowed