Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing | Zendy

Hiroshi Yamashita | Zendy; Naoshi Kuratani | Zendy; Masahito Yonezawa | Zendy; Toshihiro Ogawa | Zendy; Hiroki Nagai | Zendy; Keisuke Asai | Zendy; Shigeru Obayashi | Zendy

AI Assistant Blog Pricing

Home ZAIA Blog

Open Access

Wind Tunnel Testing on Start/Unstart Characteristics of Finite Supersonic Biplane Wing

Author(s) -

Hiroshi Yamashita,

Naoshi Kuratani,

Masahito Yonezawa,

Toshihiro Ogawa,

Hiroki Nagai,

Keisuke Asai,

Shigeru Obayashi

Publication year - 2013

Publication title -

international journal of aerospace engineering

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.361

H-Index - 22

eISSN - 1687-5974

pISSN - 1687-5966

DOI - 10.1155/2013/231434

Subject(s) - biplane , algorithm , computer science , materials science , composite material

This study describes the start/unstart characteristics of a finite and rectangular supersonic biplane wing. Two wing models were tested in wind tunnels with aspect ratios of 0.75 (model A) and 2.5 (model B). The models were composed of a Busemann biplane section. The tests were carried out using supersonic and transonic wind tunnels over a Mach number range of 0.3≤M∞≤2.3 with angles of attack of 0°, 2°, and 4°. The Schlieren system was used to observe the flow characteristics around the models. The experimental results showed that these models had start/unstart characteristics that differed from those of the Busemann biplane (two dimensional) owing to three-dimensional effects. Models A and B started at lower Mach numbers than the Busemann biplane. The characteristics also varied with aspect ratio: model A (1.3

The content you want is available to Zendy users.

Already have an account? Click here to sign in.

Having issues? You can contact us here

Accelerating Research