导航
ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1997, Vol. 18 ›› Issue (4): 455-457.
Previous Articles Next Articles
Yang Hongwei, Gao Ge
Received:
Revised:
Online:
Published:
Abstract:
A novel boundary control technique was investigated for its drag reduction abilities, which is a special surface structrure——the concave spherical pits with arranging in the order of a rhombus. The water tunnel experiment indicated that this kind of surface structure on the NACA 16012 foil surface can reduce the flow resistance up to 22%.
Key words: boundary layer control, turbulent drag reduction, water tunnel experiment
CLC Number:
V211.4
Yang Hongwei;Gao Ge . EXPERIMENTAL STUDY FOR TURBULENT DRAG REDUCTION USING A NOVEL BOUNDARY CONTROL TECHNIQUE[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(4): 455-457.
0 / / Recommend
Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks
URL: https://hkxb.buaa.edu.cn/EN/
https://hkxb.buaa.edu.cn/EN/Y1997/V18/I4/455
CJA
