日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
川崎3.5m低速風胴について
高島 勢記清原 浩洋
著者情報
ジャーナル フリー

1971 年 19 巻 206 号 p. 88-94

詳細
抄録

This paper presents a description of the new Kawasaki 3.5m low speed wind tunnel in Aircraft Division, Kawasaki Heavy Industries, Ltd. The wind tunnel has two way uses, 3.5m octagonal closed type test section and 2.5m octagonal open type test section. The maximum wind velocity is 35m/s in the former use and 65m/s in the latter, respectively. The conditions of the airflow is satisfactory. The uniformity of the velocity distribution has been ascertained to be within 2.0% in closed and 0.5% in open type, respectively. It is equipped with apparatuses such as pyramidal type six-component external balance, measured data processing systems, etc.

著者関連情報
© The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top